Application of Novel Measurement and Computational Techniques on Investigation of Air Flow in Ventilation Systems of Energy Extremely Efficient (“Passive”) Buildings

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Application of Novel Measurement and Computational Techniques on Investigation of Air Flow in Ventilation Systems of Energy Extremely Efficient (“Passive”) Buildings (en)
Примена савремених мерних и прорачунских техника за изучавање струјних параметара вентилационих система на моделу енергетски изузетно ефикасног (пасивног) објекта (sr)
Primena savremenih mernih i proračunskih tehnika za izučavanje strujnih parametara ventilacionih sistema na modelu energetski izuzetno efikasnog (pasivnog) objekta (sr_RS)
Authors

Publications

Experimental and numerical research of the flow inside the control valves trim

Ilić, Dejan; Janković, Novica; Čantrak, Đorđe; Savić, Ljubomir

(VINČA Institute of Nuclear Sciences, 2023)

TY  - JOUR
AU  - Ilić, Dejan
AU  - Janković, Novica
AU  - Čantrak, Đorđe
AU  - Savić, Ljubomir
PY  - 2023
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6994
AB  - In this paper are presented desing, testing and numerical analysis for two manufactured control valve trims. Valve trim is consisted of cage or dick stack, plug, stem and seat. Size from app. 15.88 mm (0.625 in) up to 101.6 mm (4 in) is suitable for 3D metal and plastic print, what is presented in this paper. Selective laser melting 3D metal printing is applied on the disc presented in this paper. Even better material properties from rest of the valve parts could be obtained. This is of great importance for valve retrofitting. In this paper is presented, also, new developed channel geometry, what is followed by various fluid flow phenomena. Measurement results for second prototype manufactured by 3D printing using plastics are presented in details. Here is shown, in short, procedure for determination of KV values of the test valves according to the EN 60534-2-3, Industrial-process control valves - Part 2-3: Flow capacity - Test procedures. In addition, some aspects of CFD calculations are presented.
PB  - VINČA Institute of Nuclear Sciences
T2  - Thermal Science
T1  - Experimental and numerical research of the flow inside the control valves trim
IS  - 00
SP  - 157
DO  - 10.2298/TSCI230405157I
ER  - 
@article{
author = "Ilić, Dejan and Janković, Novica and Čantrak, Đorđe and Savić, Ljubomir",
year = "2023",
abstract = "In this paper are presented desing, testing and numerical analysis for two manufactured control valve trims. Valve trim is consisted of cage or dick stack, plug, stem and seat. Size from app. 15.88 mm (0.625 in) up to 101.6 mm (4 in) is suitable for 3D metal and plastic print, what is presented in this paper. Selective laser melting 3D metal printing is applied on the disc presented in this paper. Even better material properties from rest of the valve parts could be obtained. This is of great importance for valve retrofitting. In this paper is presented, also, new developed channel geometry, what is followed by various fluid flow phenomena. Measurement results for second prototype manufactured by 3D printing using plastics are presented in details. Here is shown, in short, procedure for determination of KV values of the test valves according to the EN 60534-2-3, Industrial-process control valves - Part 2-3: Flow capacity - Test procedures. In addition, some aspects of CFD calculations are presented.",
publisher = "VINČA Institute of Nuclear Sciences",
journal = "Thermal Science",
title = "Experimental and numerical research of the flow inside the control valves trim",
number = "00",
pages = "157",
doi = "10.2298/TSCI230405157I"
}
Ilić, D., Janković, N., Čantrak, Đ.,& Savić, L.. (2023). Experimental and numerical research of the flow inside the control valves trim. in Thermal Science
VINČA Institute of Nuclear Sciences.(00), 157.
https://doi.org/10.2298/TSCI230405157I
Ilić D, Janković N, Čantrak Đ, Savić L. Experimental and numerical research of the flow inside the control valves trim. in Thermal Science. 2023;(00):157.
doi:10.2298/TSCI230405157I .
Ilić, Dejan, Janković, Novica, Čantrak, Đorđe, Savić, Ljubomir, "Experimental and numerical research of the flow inside the control valves trim" in Thermal Science, no. 00 (2023):157,
https://doi.org/10.2298/TSCI230405157I . .

Enstrophy Study of the Turbulent Swirling Flow in Pipe

Čantrak, Đorđe; Janković, Novica; Ilić, Dejan; Lečić, Lazar

(Српско друштво за механику, 2023)

TY  - CONF
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Ilić, Dejan
AU  - Lečić, Lazar
PY  - 2023
UR  - http://www.ssm.kg.ac.rs/congress_2023/papers/
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6911
UR  - http://www.ssm.kg.ac.rs/congress_2023/wp-content/uploads/upload/ICSSM2023_Book_of_Proceedings.pdf
AB  - Turbulent swirling flow is characterized by significant vortex fluctuations, intensive diffusion processes and energy cascade transfer from larger to smaller vortices over a continuous spectrum of wave numbers. The dissipation of the kinetic energy of turbulence occurs in the smallest vortices, because in these areas, both the velocity gradients and the deformation velocities are the largest. In this paper is analyzed turbulent swirling flow in pipe, generated by the axial fan impellers for three various blade angles (22°, 26° and 30°). Vorticity, enstrophy and lambda 2 values are calculated in order to study the structure of the generated turbulent swirling flows. Axial fan impeller operates in the region of lower flow rates, and it is shown that blade angle doesn’t influence much on the integral flow parameters, as well as on the enstrophy distribution. It is, also, shown that the dissipation of the kinetic energy of turbulence is associated with the vorticity fluctuations, i.e. with turbulent fluctuating enstrophy. All these distributions are obtained by use of the high speed particle image velocimetry data and provided velocity fields. Enstrophy is directly related to the kinetic energy, i.e. it corresponds to dissipation effects in this flow. It has maximum in small vortices, i.e. in shear layer, that surrounds vortex core region, where the process of turbulence kinetic energy dissipation occurs.
PB  - Српско друштво за механику
C3  - 9th International Congress of the Serbian Society of Mechanics July 5-7, 2023, Vrnjačka Banja, Serbia
T1  - Enstrophy Study of the Turbulent Swirling Flow in Pipe
SP  - 84
UR  - https://hdl.handle.net/21.15107/rcub_machinery_6911
ER  - 
@conference{
author = "Čantrak, Đorđe and Janković, Novica and Ilić, Dejan and Lečić, Lazar",
year = "2023",
abstract = "Turbulent swirling flow is characterized by significant vortex fluctuations, intensive diffusion processes and energy cascade transfer from larger to smaller vortices over a continuous spectrum of wave numbers. The dissipation of the kinetic energy of turbulence occurs in the smallest vortices, because in these areas, both the velocity gradients and the deformation velocities are the largest. In this paper is analyzed turbulent swirling flow in pipe, generated by the axial fan impellers for three various blade angles (22°, 26° and 30°). Vorticity, enstrophy and lambda 2 values are calculated in order to study the structure of the generated turbulent swirling flows. Axial fan impeller operates in the region of lower flow rates, and it is shown that blade angle doesn’t influence much on the integral flow parameters, as well as on the enstrophy distribution. It is, also, shown that the dissipation of the kinetic energy of turbulence is associated with the vorticity fluctuations, i.e. with turbulent fluctuating enstrophy. All these distributions are obtained by use of the high speed particle image velocimetry data and provided velocity fields. Enstrophy is directly related to the kinetic energy, i.e. it corresponds to dissipation effects in this flow. It has maximum in small vortices, i.e. in shear layer, that surrounds vortex core region, where the process of turbulence kinetic energy dissipation occurs.",
publisher = "Српско друштво за механику",
journal = "9th International Congress of the Serbian Society of Mechanics July 5-7, 2023, Vrnjačka Banja, Serbia",
title = "Enstrophy Study of the Turbulent Swirling Flow in Pipe",
pages = "84",
url = "https://hdl.handle.net/21.15107/rcub_machinery_6911"
}
Čantrak, Đ., Janković, N., Ilić, D.,& Lečić, L.. (2023). Enstrophy Study of the Turbulent Swirling Flow in Pipe. in 9th International Congress of the Serbian Society of Mechanics July 5-7, 2023, Vrnjačka Banja, Serbia
Српско друштво за механику., 84.
https://hdl.handle.net/21.15107/rcub_machinery_6911
Čantrak Đ, Janković N, Ilić D, Lečić L. Enstrophy Study of the Turbulent Swirling Flow in Pipe. in 9th International Congress of the Serbian Society of Mechanics July 5-7, 2023, Vrnjačka Banja, Serbia. 2023;:84.
https://hdl.handle.net/21.15107/rcub_machinery_6911 .
Čantrak, Đorđe, Janković, Novica, Ilić, Dejan, Lečić, Lazar, "Enstrophy Study of the Turbulent Swirling Flow in Pipe" in 9th International Congress of the Serbian Society of Mechanics July 5-7, 2023, Vrnjačka Banja, Serbia (2023):84,
https://hdl.handle.net/21.15107/rcub_machinery_6911 .

Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model

Raković, Milan; Radenković, Darko; Ćoćić, Aleksandar; Lečić, Milan

(Sage Publications Ltd, London, 2022)

TY  - JOUR
AU  - Raković, Milan
AU  - Radenković, Darko
AU  - Ćoćić, Aleksandar
AU  - Lečić, Milan
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3693
AB  - In this work, numerical simulations of upward turbulent bubbly flows in vertical pipes are conducted in the Euler-Euler framework with a low-Reynolds-number (LRN) model for liquid. It is found that the existing correlation for the drag coefficient of a single bubble in a shear flow, which has been successfully used along with the high-Reynolds-number (HRN) models, cannot be used with the LRN model. The reason is that drag forces of bubbles calculated using such correlation are enormous in near-wall cells (order of 10(12) N/m(3)), which causes a divergence of numerical simulations with LRN. Therefore, a modified correlation for the drag coefficient of a single bubble in shear flow, that can be used successfully with the LRN model, has been proposed. The results of numerical simulations, performed with a new correlation for the drag coefficient, are analysed and compared to selected experimental measurements for different pipe diameters and different flow conditions of gas and liquid. It is shown that the largest effect of the application of the new correlation for the drag coefficient of a single bubble in shear flow in numerical simulations can be achieved on the reduction of the relative velocity between gas and liquid. The degree of this reduction depends on the pipe diameter and liquid volumetric flux.
PB  - Sage Publications Ltd, London
T2  - Advances in Mechanical Engineering
T1  - Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model
IS  - 4
VL  - 14
DO  - 10.1177/16878132221094909
ER  - 
@article{
author = "Raković, Milan and Radenković, Darko and Ćoćić, Aleksandar and Lečić, Milan",
year = "2022",
abstract = "In this work, numerical simulations of upward turbulent bubbly flows in vertical pipes are conducted in the Euler-Euler framework with a low-Reynolds-number (LRN) model for liquid. It is found that the existing correlation for the drag coefficient of a single bubble in a shear flow, which has been successfully used along with the high-Reynolds-number (HRN) models, cannot be used with the LRN model. The reason is that drag forces of bubbles calculated using such correlation are enormous in near-wall cells (order of 10(12) N/m(3)), which causes a divergence of numerical simulations with LRN. Therefore, a modified correlation for the drag coefficient of a single bubble in shear flow, that can be used successfully with the LRN model, has been proposed. The results of numerical simulations, performed with a new correlation for the drag coefficient, are analysed and compared to selected experimental measurements for different pipe diameters and different flow conditions of gas and liquid. It is shown that the largest effect of the application of the new correlation for the drag coefficient of a single bubble in shear flow in numerical simulations can be achieved on the reduction of the relative velocity between gas and liquid. The degree of this reduction depends on the pipe diameter and liquid volumetric flux.",
publisher = "Sage Publications Ltd, London",
journal = "Advances in Mechanical Engineering",
title = "Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model",
number = "4",
volume = "14",
doi = "10.1177/16878132221094909"
}
Raković, M., Radenković, D., Ćoćić, A.,& Lečić, M.. (2022). Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model. in Advances in Mechanical Engineering
Sage Publications Ltd, London., 14(4).
https://doi.org/10.1177/16878132221094909
Raković M, Radenković D, Ćoćić A, Lečić M. Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model. in Advances in Mechanical Engineering. 2022;14(4).
doi:10.1177/16878132221094909 .
Raković, Milan, Radenković, Darko, Ćoćić, Aleksandar, Lečić, Milan, "Euler-Euler numerical simulations of upward turbulent bubbly flows in vertical pipes with low-Reynolds-number model" in Advances in Mechanical Engineering, 14, no. 4 (2022),
https://doi.org/10.1177/16878132221094909 . .

LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet

Čantrak, Đorđe; Janković, Novica; Ilić, Dejan; Nedeljković, Miloš

(2022)

TY  - CONF
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Ilić, Dejan
AU  - Nedeljković, Miloš
PY  - 2022
UR  - https://www.iahr.org/library/infor?pid=21378
UR  - https://cmswebonline.com/iahr2022/epro/html/06-08-039-1817.xml
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5573
AB  - Turbulent swirling flow occupies attention of numerous researchers worldwide. In this paper are presented experimental results of the research of the self induced pre-swirl by the centrifugal impeller. Circumferential velocity was measured in two cross-sections by use of the one-component laser Doppler velocimetry (LDV) system. Flow visualization at the pump inlet, as well as at the pump outlet, was conducted by using the high speed camera Photron Fastcam SA1.1 and the LED light for illumination. Air bubbles were used for flow illumination, and silver coated particles for LDV measurements. Pump characteristics (head, volume flow rate and power) are, also, measured in the tested duty point. Pre-swirl is visualized, while almost developed uniform turbulent flow is documented at the pump casing outlet. By using LDV it was possible to identify almost solid body circumferential velocity profile at the pump inlet, only 0.5D upstream, where D is pipe inner diameter. So, the influence of the impeller suction is obvious. In paper is, also discussed statistics of the generated turbulence.
C3  - 39th IAHR World Congress, Proceedings, Ed.: Miguel Ortega-Sánchez, No. 06-08-039-1817, June 19-24th, Granada, Spain
T1  - LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet
EP  - 5270
SP  - 5264
DO  - 10.3850/IAHR-39WC2521711920221817
ER  - 
@conference{
author = "Čantrak, Đorđe and Janković, Novica and Ilić, Dejan and Nedeljković, Miloš",
year = "2022",
abstract = "Turbulent swirling flow occupies attention of numerous researchers worldwide. In this paper are presented experimental results of the research of the self induced pre-swirl by the centrifugal impeller. Circumferential velocity was measured in two cross-sections by use of the one-component laser Doppler velocimetry (LDV) system. Flow visualization at the pump inlet, as well as at the pump outlet, was conducted by using the high speed camera Photron Fastcam SA1.1 and the LED light for illumination. Air bubbles were used for flow illumination, and silver coated particles for LDV measurements. Pump characteristics (head, volume flow rate and power) are, also, measured in the tested duty point. Pre-swirl is visualized, while almost developed uniform turbulent flow is documented at the pump casing outlet. By using LDV it was possible to identify almost solid body circumferential velocity profile at the pump inlet, only 0.5D upstream, where D is pipe inner diameter. So, the influence of the impeller suction is obvious. In paper is, also discussed statistics of the generated turbulence.",
journal = "39th IAHR World Congress, Proceedings, Ed.: Miguel Ortega-Sánchez, No. 06-08-039-1817, June 19-24th, Granada, Spain",
title = "LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet",
pages = "5270-5264",
doi = "10.3850/IAHR-39WC2521711920221817"
}
Čantrak, Đ., Janković, N., Ilić, D.,& Nedeljković, M.. (2022). LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet. in 39th IAHR World Congress, Proceedings, Ed.: Miguel Ortega-Sánchez, No. 06-08-039-1817, June 19-24th, Granada, Spain, 5264-5270.
https://doi.org/10.3850/IAHR-39WC2521711920221817
Čantrak Đ, Janković N, Ilić D, Nedeljković M. LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet. in 39th IAHR World Congress, Proceedings, Ed.: Miguel Ortega-Sánchez, No. 06-08-039-1817, June 19-24th, Granada, Spain. 2022;:5264-5270.
doi:10.3850/IAHR-39WC2521711920221817 .
Čantrak, Đorđe, Janković, Novica, Ilić, Dejan, Nedeljković, Miloš, "LDV Investigation of the Self Induced Pre-Swirl and Flow Visualization at the Centrifugal Pump Inlet and Outlet" in 39th IAHR World Congress, Proceedings, Ed.: Miguel Ortega-Sánchez, No. 06-08-039-1817, June 19-24th, Granada, Spain (2022):5264-5270,
https://doi.org/10.3850/IAHR-39WC2521711920221817 . .
1

High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe

Čantrak, Đorđe; Janković, Novica

(SAGE JOURNALS, 2022)

TY  - JOUR
AU  - Čantrak, Đorđe
AU  - Janković, Novica
PY  - 2022
UR  - https://journals.sagepub.com/doi/10.1177/16878132221130563
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6338
AB  - Investigation of the turbulent swirl flow in the piping system is one of the most complex investigations in the field of energetics and turbulence. Axial fans in a pipe, without guide vanes, are widely used in practice and the problem of their duty point and energy efficiency is still extensively discussed. Analysis of the interaction between axial fans energy and construction parameters is one of the main topics in defining the fans energy efficiency potential. On one side, there is a three-dimensional velocity field in the wall-bounded flow with regions of great turbulence intensity. On the other side, there is a complex blade geometry, which generates the turbulent swirl flow. This paper presents research on the turbulent swirl flow, Rankine type, in an axially restricted system, using high-speed stereo particle image velocimetry (HSS PIV). Axial fan impeller, with outer diameter 0.399 m and nine twisted blades is the flow generator. The Reynolds number Re = 176,529 is achieved in the pipe. Reynolds stresses, statistical moments of higher order, and invariant maps are calculated based on the three component velocity fields. Here, intensive changes of all statistical parameters occur in radial and axial direction. In the flow region, four flow regions can be identified. Interaction of all these four flow regions produces extremely complex turbulent swirl flow, which is generated behind the axial fans. Determined invariant maps reveal turbulence structure. It is shown that the state of turbulence on the pipe axis is three-component isotropic, which is contrary to the case of axially unrestricted turbulent swirl flows. In the rest of the space, in the region up to r/R = 0.52, the states of turbulence occur in the area in between the boundaries which designate axis-symmetric turbulence (contraction) and axis-symmetric turbulence (expansion), in the vicinity of the state of three-component isotropic turbulence.
PB  - SAGE JOURNALS
T2  - Advances in Mechanical Engineering
T1  - High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe
VL  - 14
DO  - 10.1177/16878132221130563
ER  - 
@article{
author = "Čantrak, Đorđe and Janković, Novica",
year = "2022",
abstract = "Investigation of the turbulent swirl flow in the piping system is one of the most complex investigations in the field of energetics and turbulence. Axial fans in a pipe, without guide vanes, are widely used in practice and the problem of their duty point and energy efficiency is still extensively discussed. Analysis of the interaction between axial fans energy and construction parameters is one of the main topics in defining the fans energy efficiency potential. On one side, there is a three-dimensional velocity field in the wall-bounded flow with regions of great turbulence intensity. On the other side, there is a complex blade geometry, which generates the turbulent swirl flow. This paper presents research on the turbulent swirl flow, Rankine type, in an axially restricted system, using high-speed stereo particle image velocimetry (HSS PIV). Axial fan impeller, with outer diameter 0.399 m and nine twisted blades is the flow generator. The Reynolds number Re = 176,529 is achieved in the pipe. Reynolds stresses, statistical moments of higher order, and invariant maps are calculated based on the three component velocity fields. Here, intensive changes of all statistical parameters occur in radial and axial direction. In the flow region, four flow regions can be identified. Interaction of all these four flow regions produces extremely complex turbulent swirl flow, which is generated behind the axial fans. Determined invariant maps reveal turbulence structure. It is shown that the state of turbulence on the pipe axis is three-component isotropic, which is contrary to the case of axially unrestricted turbulent swirl flows. In the rest of the space, in the region up to r/R = 0.52, the states of turbulence occur in the area in between the boundaries which designate axis-symmetric turbulence (contraction) and axis-symmetric turbulence (expansion), in the vicinity of the state of three-component isotropic turbulence.",
publisher = "SAGE JOURNALS",
journal = "Advances in Mechanical Engineering",
title = "High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe",
volume = "14",
doi = "10.1177/16878132221130563"
}
Čantrak, Đ.,& Janković, N.. (2022). High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe. in Advances in Mechanical Engineering
SAGE JOURNALS., 14.
https://doi.org/10.1177/16878132221130563
Čantrak Đ, Janković N. High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe. in Advances in Mechanical Engineering. 2022;14.
doi:10.1177/16878132221130563 .
Čantrak, Đorđe, Janković, Novica, "High Speed Stereo PIV Investigation of the Turbuelnce Structure of the Axially Restricted Turbulent Swirl Flow behind the Axial Fan in Pipe" in Advances in Mechanical Engineering, 14 (2022),
https://doi.org/10.1177/16878132221130563 . .
1

Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data

Čantrak, Đorđe; Janković, Novica

(MDPI, 2022)

TY  - JOUR
AU  - Čantrak, Đorđe
AU  - Janković, Novica
PY  - 2022
UR  - https://www.mdpi.com/1996-1073/15/15/5417
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6336
AB  - Turbulent swirl flow, which exists in numerous turbomachinery systems, is the focus of
this paper. It consumes a significant amount of energy, so it is a subject of investigation for many
researchers. It is even more present in ventilation systems, as numerous axial fans are still installed without guide vanes. The experimental investigation of the turbulent swirl flow behind an axial fan in a pipe, installed in a test rig with a free inlet and ducted outlet, as defined in the international standard ISO 5801, is presented in this paper. Moreover, in this paper, the axially restricted case is studied. A designed axial fan generates a Rankine vortex with a complex structure, and research on the vortex turbulence structure and dynamics is presented. On the basis of the HSS PIV (high-speed stereo particle image velocimetry), measurement results are calculated using invariant maps. All states of turbulence anisotropy are thoroughly analyzed by applying the invariant theory on HSS PIV results. Vortex dynamics is observed on the basis of the total velocity minima positions and their repetitions. Both methods are correlated, and important conclusions regarding vortex behavior are deduced.
PB  - MDPI
T2  - Energies
T1  - Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data
VL  - 15
DO  - 10.3390/en15155417
ER  - 
@article{
author = "Čantrak, Đorđe and Janković, Novica",
year = "2022",
abstract = "Turbulent swirl flow, which exists in numerous turbomachinery systems, is the focus of
this paper. It consumes a significant amount of energy, so it is a subject of investigation for many
researchers. It is even more present in ventilation systems, as numerous axial fans are still installed without guide vanes. The experimental investigation of the turbulent swirl flow behind an axial fan in a pipe, installed in a test rig with a free inlet and ducted outlet, as defined in the international standard ISO 5801, is presented in this paper. Moreover, in this paper, the axially restricted case is studied. A designed axial fan generates a Rankine vortex with a complex structure, and research on the vortex turbulence structure and dynamics is presented. On the basis of the HSS PIV (high-speed stereo particle image velocimetry), measurement results are calculated using invariant maps. All states of turbulence anisotropy are thoroughly analyzed by applying the invariant theory on HSS PIV results. Vortex dynamics is observed on the basis of the total velocity minima positions and their repetitions. Both methods are correlated, and important conclusions regarding vortex behavior are deduced.",
publisher = "MDPI",
journal = "Energies",
title = "Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data",
volume = "15",
doi = "10.3390/en15155417"
}
Čantrak, Đ.,& Janković, N.. (2022). Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data. in Energies
MDPI., 15.
https://doi.org/10.3390/en15155417
Čantrak Đ, Janković N. Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data. in Energies. 2022;15.
doi:10.3390/en15155417 .
Čantrak, Đorđe, Janković, Novica, "Turbulence Structure and Dynamics Investigation of Turbulent Swirl Flow in Pipe Using High-Speed Stereo PIV Data" in Energies, 15 (2022),
https://doi.org/10.3390/en15155417 . .
3
4

Experimental Аnd Numerical Investigation of Ball Valve Characteristics

Raković, Milan; Lečić, Lazar; Ćoćić, Aleksandar; Janković, Novica

(2022)

TY  - CONF
AU  - Raković, Milan
AU  - Lečić, Lazar
AU  - Ćoćić, Aleksandar
AU  - Janković, Novica
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6276
C3  - Full Paper Proceedings International Conference IEEP2022
T1  - Experimental Аnd Numerical Investigation of Ball Valve Characteristics
SP  - 252
UR  - https://hdl.handle.net/21.15107/rcub_machinery_6276
ER  - 
@conference{
author = "Raković, Milan and Lečić, Lazar and Ćoćić, Aleksandar and Janković, Novica",
year = "2022",
journal = "Full Paper Proceedings International Conference IEEP2022",
title = "Experimental Аnd Numerical Investigation of Ball Valve Characteristics",
pages = "252",
url = "https://hdl.handle.net/21.15107/rcub_machinery_6276"
}
Raković, M., Lečić, L., Ćoćić, A.,& Janković, N.. (2022). Experimental Аnd Numerical Investigation of Ball Valve Characteristics. in Full Paper Proceedings International Conference IEEP2022, 252.
https://hdl.handle.net/21.15107/rcub_machinery_6276
Raković M, Lečić L, Ćoćić A, Janković N. Experimental Аnd Numerical Investigation of Ball Valve Characteristics. in Full Paper Proceedings International Conference IEEP2022. 2022;:252.
https://hdl.handle.net/21.15107/rcub_machinery_6276 .
Raković, Milan, Lečić, Lazar, Ćoćić, Aleksandar, Janković, Novica, "Experimental Аnd Numerical Investigation of Ball Valve Characteristics" in Full Paper Proceedings International Conference IEEP2022 (2022):252,
https://hdl.handle.net/21.15107/rcub_machinery_6276 .

Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows

Raković, Milan; Radenković, Darko; Ćoćić, Aleksandar; Lečić, Milan

(2022)

TY  - CONF
AU  - Raković, Milan
AU  - Radenković, Darko
AU  - Ćoćić, Aleksandar
AU  - Lečić, Milan
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6219
AB  - Numerical simulations of upward turbulent bubbly flows in vertical pipes are carried
out in the Euler-Euler framework with a low-Reynolds-number (LRN) model for liquid for
various flow conditions. It is found that the correlation for the drag coefficient of a single
bubble in a shear flow, which has been successfully used in numerical simulations with
the high-Reynolds-number (HRN) models, cannot be used with the LRN model. The
reason is an excessive value of drag coefficient of a single bubble in the near-wall cells.
Therefore, a new correlation for the drag coefficient of a single bubble in shear flow has
been proposed. The results of numerical simulations are analysed and compared to
selected experiment results. It is shown that the largest effect of the application of the
new correlation for the drag coefficient of a single bubble in shear flow can be achieved
on the reduction of the relative velocity between gas and liquid. Overall, the results of
numerical simulations agree well with the experimental results.
C3  - ICAS 2022 Book of abstracts
T1  - Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows
SP  - 85
UR  - https://hdl.handle.net/21.15107/rcub_machinery_6219
ER  - 
@conference{
author = "Raković, Milan and Radenković, Darko and Ćoćić, Aleksandar and Lečić, Milan",
year = "2022",
abstract = "Numerical simulations of upward turbulent bubbly flows in vertical pipes are carried
out in the Euler-Euler framework with a low-Reynolds-number (LRN) model for liquid for
various flow conditions. It is found that the correlation for the drag coefficient of a single
bubble in a shear flow, which has been successfully used in numerical simulations with
the high-Reynolds-number (HRN) models, cannot be used with the LRN model. The
reason is an excessive value of drag coefficient of a single bubble in the near-wall cells.
Therefore, a new correlation for the drag coefficient of a single bubble in shear flow has
been proposed. The results of numerical simulations are analysed and compared to
selected experiment results. It is shown that the largest effect of the application of the
new correlation for the drag coefficient of a single bubble in shear flow can be achieved
on the reduction of the relative velocity between gas and liquid. Overall, the results of
numerical simulations agree well with the experimental results.",
journal = "ICAS 2022 Book of abstracts",
title = "Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows",
pages = "85",
url = "https://hdl.handle.net/21.15107/rcub_machinery_6219"
}
Raković, M., Radenković, D., Ćoćić, A.,& Lečić, M.. (2022). Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows. in ICAS 2022 Book of abstracts, 85.
https://hdl.handle.net/21.15107/rcub_machinery_6219
Raković M, Radenković D, Ćoćić A, Lečić M. Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows. in ICAS 2022 Book of abstracts. 2022;:85.
https://hdl.handle.net/21.15107/rcub_machinery_6219 .
Raković, Milan, Radenković, Darko, Ćoćić, Aleksandar, Lečić, Milan, "Influence of the drag coefficient of a single bubble in vertical upward turbulent bubbly flows" in ICAS 2022 Book of abstracts (2022):85,
https://hdl.handle.net/21.15107/rcub_machinery_6219 .

Solar updraft tower technology as clean and renewable energy source

Ćoćić, Aleksandar

(2022)

TY  - CONF
AU  - Ćoćić, Aleksandar
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5527
AB  - Solar energy is renewable, clean and practically non-depletable energy source - it is estimated that we will have steady, unlimited supply of sunlight for another 5 billion years. Efficient utilization of solar energy and development of solar systems in that purpose are the research topics of many scientists  and engineers worldwide. Solar updraft tower (SUT) technology is attracting interest in many regions worldwide, being a compelling prospect for producing  clean and renewable energy.  Very import operational parameters of SUT systems are mass flow rate and pressure difference inside the tower. Based on the  assumption of one-dimensional (1D) flow, a comprehensive mathematical model for buoyancy driven air flow inside the SUT power plant is developed. It consists of system of nonlinear differential equations which describes the flow inside collector and the tower, and algebraic equations which describes the flow in collector to tower transition section and turbines. Validity of the model is confirmed by numerical solution of the equations for the case of Manzaneres SUT, where good agreement is found between obtained solution and available experimental data. Dimensionless form of model equations are further developed which enables the performance analysis of SUT systems. It is found that only large-scale systems are feasible, and that increase in tower height increase the mass flow rate only to some extent. Additionally, CFD computations based on Boussinesq model for
buoyancy-driven flow and  using Reynold-Averaged Navier-Stokes (RANS) equations are performed where good agreement is found with derived 1D model.
C3  - Proceedings International Conference IEEP2022, VIII Regional Conference: INDUSTRIAL ENERGY AND ENVIRONMENTAL PROTECTION IN THE COUNTRIES OF SOUTHEAST EUROPE
T1  - Solar updraft tower technology as clean and renewable energy source
EP  - 438
SP  - 424
UR  - https://hdl.handle.net/21.15107/rcub_machinery_5527
ER  - 
@conference{
author = "Ćoćić, Aleksandar",
year = "2022",
abstract = "Solar energy is renewable, clean and practically non-depletable energy source - it is estimated that we will have steady, unlimited supply of sunlight for another 5 billion years. Efficient utilization of solar energy and development of solar systems in that purpose are the research topics of many scientists  and engineers worldwide. Solar updraft tower (SUT) technology is attracting interest in many regions worldwide, being a compelling prospect for producing  clean and renewable energy.  Very import operational parameters of SUT systems are mass flow rate and pressure difference inside the tower. Based on the  assumption of one-dimensional (1D) flow, a comprehensive mathematical model for buoyancy driven air flow inside the SUT power plant is developed. It consists of system of nonlinear differential equations which describes the flow inside collector and the tower, and algebraic equations which describes the flow in collector to tower transition section and turbines. Validity of the model is confirmed by numerical solution of the equations for the case of Manzaneres SUT, where good agreement is found between obtained solution and available experimental data. Dimensionless form of model equations are further developed which enables the performance analysis of SUT systems. It is found that only large-scale systems are feasible, and that increase in tower height increase the mass flow rate only to some extent. Additionally, CFD computations based on Boussinesq model for
buoyancy-driven flow and  using Reynold-Averaged Navier-Stokes (RANS) equations are performed where good agreement is found with derived 1D model.",
journal = "Proceedings International Conference IEEP2022, VIII Regional Conference: INDUSTRIAL ENERGY AND ENVIRONMENTAL PROTECTION IN THE COUNTRIES OF SOUTHEAST EUROPE",
title = "Solar updraft tower technology as clean and renewable energy source",
pages = "438-424",
url = "https://hdl.handle.net/21.15107/rcub_machinery_5527"
}
Ćoćić, A.. (2022). Solar updraft tower technology as clean and renewable energy source. in Proceedings International Conference IEEP2022, VIII Regional Conference: INDUSTRIAL ENERGY AND ENVIRONMENTAL PROTECTION IN THE COUNTRIES OF SOUTHEAST EUROPE, 424-438.
https://hdl.handle.net/21.15107/rcub_machinery_5527
Ćoćić A. Solar updraft tower technology as clean and renewable energy source. in Proceedings International Conference IEEP2022, VIII Regional Conference: INDUSTRIAL ENERGY AND ENVIRONMENTAL PROTECTION IN THE COUNTRIES OF SOUTHEAST EUROPE. 2022;:424-438.
https://hdl.handle.net/21.15107/rcub_machinery_5527 .
Ćoćić, Aleksandar, "Solar updraft tower technology as clean and renewable energy source" in Proceedings International Conference IEEP2022, VIII Regional Conference: INDUSTRIAL ENERGY AND ENVIRONMENTAL PROTECTION IN THE COUNTRIES OF SOUTHEAST EUROPE (2022):424-438,
https://hdl.handle.net/21.15107/rcub_machinery_5527 .

Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach

Milivojević, Marija; Ćoćić, Aleksandar; Tomić, Matej

(2022)

TY  - CONF
AU  - Milivojević, Marija
AU  - Ćoćić, Aleksandar
AU  - Tomić, Matej
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5526
AB  - Air-to-liquid heat exchangers which are used in the automotive industry are of fin and tube type. In conjunction with the heat exchanger, axial fans are used, for two main reasons: to compensate the pressure drop of air and to enhance the cooling efficiency. In design process of heat exchanger, it is necessary to choose the appropriate axial fan which will meet the demands. One of the main data set in that sense is the relationship between the air volumetric flow rate and pressure drop in the heat exchanger. In this paper, air flow through the fin and tube type heat exchanger is analyzed using steady-state numerical simulations. Since it is practically impossible to generate the numerical grid for  the real, physical fins, they are modeled using the porous media approach, with Darcy-Forchheimer model, applied in defined cell zone which corresponds to fins. By this, additional sink/source term is added in momentum equation. From series of numerical computations, where the inlet flow rate is varied, the relationship between pressure drop in porous zone and flow rate is established. Flow of the air is treated as incompressible and isothermal. OpenFOAM, free and open-source software for computational fluid dynamics (CFD) is used for aforementioned computations. The control volume is modeled to match the experimental airflow test rig set up, while for the boundary conditions velocity inlet and pressure outlet are used. Symmetry boundary condition is applied at the longitudinal plane of the model, in order to reduce the mesh count. Values of coefficients in Darcy-Forchheimer model are estimated from the geometrical characteristics of the heat exchanger and available experimental data. It is concluded that porous media approach implemented in OpenFOAM software can be used as toolkit in prediction of pressure of drop from the air side in automotive heat exchanger.
C3  - First International Conference on Mathematical Modeling in Mechanics and Engineering, Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade, Serbia, 8-10 September 2022
T1  - Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach
SP  - 86
UR  - https://hdl.handle.net/21.15107/rcub_machinery_5526
ER  - 
@conference{
author = "Milivojević, Marija and Ćoćić, Aleksandar and Tomić, Matej",
year = "2022",
abstract = "Air-to-liquid heat exchangers which are used in the automotive industry are of fin and tube type. In conjunction with the heat exchanger, axial fans are used, for two main reasons: to compensate the pressure drop of air and to enhance the cooling efficiency. In design process of heat exchanger, it is necessary to choose the appropriate axial fan which will meet the demands. One of the main data set in that sense is the relationship between the air volumetric flow rate and pressure drop in the heat exchanger. In this paper, air flow through the fin and tube type heat exchanger is analyzed using steady-state numerical simulations. Since it is practically impossible to generate the numerical grid for  the real, physical fins, they are modeled using the porous media approach, with Darcy-Forchheimer model, applied in defined cell zone which corresponds to fins. By this, additional sink/source term is added in momentum equation. From series of numerical computations, where the inlet flow rate is varied, the relationship between pressure drop in porous zone and flow rate is established. Flow of the air is treated as incompressible and isothermal. OpenFOAM, free and open-source software for computational fluid dynamics (CFD) is used for aforementioned computations. The control volume is modeled to match the experimental airflow test rig set up, while for the boundary conditions velocity inlet and pressure outlet are used. Symmetry boundary condition is applied at the longitudinal plane of the model, in order to reduce the mesh count. Values of coefficients in Darcy-Forchheimer model are estimated from the geometrical characteristics of the heat exchanger and available experimental data. It is concluded that porous media approach implemented in OpenFOAM software can be used as toolkit in prediction of pressure of drop from the air side in automotive heat exchanger.",
journal = "First International Conference on Mathematical Modeling in Mechanics and Engineering, Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade, Serbia, 8-10 September 2022",
title = "Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach",
pages = "86",
url = "https://hdl.handle.net/21.15107/rcub_machinery_5526"
}
Milivojević, M., Ćoćić, A.,& Tomić, M.. (2022). Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach. in First International Conference on Mathematical Modeling in Mechanics and Engineering, Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade, Serbia, 8-10 September 2022, 86.
https://hdl.handle.net/21.15107/rcub_machinery_5526
Milivojević M, Ćoćić A, Tomić M. Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach. in First International Conference on Mathematical Modeling in Mechanics and Engineering, Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade, Serbia, 8-10 September 2022. 2022;:86.
https://hdl.handle.net/21.15107/rcub_machinery_5526 .
Milivojević, Marija, Ćoćić, Aleksandar, Tomić, Matej, "Analysis of Pressure Drop From The Air Side in Automotive Heat Exchanger Using Porous Media Approach" in First International Conference on Mathematical Modeling in Mechanics and Engineering, Mathematical Institute of the Serbian Academy of Sciences and Arts, Belgrade, Serbia, 8-10 September 2022 (2022):86,
https://hdl.handle.net/21.15107/rcub_machinery_5526 .

Numerical Computations of Elastic Torsion Using the Finite-Volume Method

Ćoćić, Aleksandar

(2022)

TY  - CONF
AU  - Ćoćić, Aleksandar
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5525
AB  - Finite volume method is predominantly used in computational fluid dynamics (CFD), and it is very rarely used in computational solid mechanics. But essentially, it is just one approach for numerical solution of PDEs (FVM discretises strong conservative form of momentum equation, while FEM uses weak form). OpenFOAM, free and open-source CFD software is used as the tool for implementation of numerical solutions  of equations (a), (b) and (c). General FVM solver, based on the (a) is implemented using OpenFOAM libraries, together with appropriate Neumann BC. The solver is then tested on many examples, starting from the problems with known analytical solution (excellent agreement is found). Additional post-processing is implemented within the solver, where after determination of shear stress (calculated from the gradient of warping function field), Prandtl stress function is calculated as the stream function of stress vector field. It is shown that boundary-fitted grid which is characteristic for FVM is very suited for considered computations.  Finally, analogy between elastic torsion and some classical fluid mechanics problems governed with the same type of the equations is analyzed.
C3  - First International Conference on Mathematical Modeling in Mechanics and Engineering
T1  - Numerical Computations of Elastic Torsion Using the Finite-Volume Method
SP  - 120
UR  - https://hdl.handle.net/21.15107/rcub_machinery_5525
ER  - 
@conference{
author = "Ćoćić, Aleksandar",
year = "2022",
abstract = "Finite volume method is predominantly used in computational fluid dynamics (CFD), and it is very rarely used in computational solid mechanics. But essentially, it is just one approach for numerical solution of PDEs (FVM discretises strong conservative form of momentum equation, while FEM uses weak form). OpenFOAM, free and open-source CFD software is used as the tool for implementation of numerical solutions  of equations (a), (b) and (c). General FVM solver, based on the (a) is implemented using OpenFOAM libraries, together with appropriate Neumann BC. The solver is then tested on many examples, starting from the problems with known analytical solution (excellent agreement is found). Additional post-processing is implemented within the solver, where after determination of shear stress (calculated from the gradient of warping function field), Prandtl stress function is calculated as the stream function of stress vector field. It is shown that boundary-fitted grid which is characteristic for FVM is very suited for considered computations.  Finally, analogy between elastic torsion and some classical fluid mechanics problems governed with the same type of the equations is analyzed.",
journal = "First International Conference on Mathematical Modeling in Mechanics and Engineering",
title = "Numerical Computations of Elastic Torsion Using the Finite-Volume Method",
pages = "120",
url = "https://hdl.handle.net/21.15107/rcub_machinery_5525"
}
Ćoćić, A.. (2022). Numerical Computations of Elastic Torsion Using the Finite-Volume Method. in First International Conference on Mathematical Modeling in Mechanics and Engineering, 120.
https://hdl.handle.net/21.15107/rcub_machinery_5525
Ćoćić A. Numerical Computations of Elastic Torsion Using the Finite-Volume Method. in First International Conference on Mathematical Modeling in Mechanics and Engineering. 2022;:120.
https://hdl.handle.net/21.15107/rcub_machinery_5525 .
Ćoćić, Aleksandar, "Numerical Computations of Elastic Torsion Using the Finite-Volume Method" in First International Conference on Mathematical Modeling in Mechanics and Engineering (2022):120,
https://hdl.handle.net/21.15107/rcub_machinery_5525 .

Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube

Burazer, Jela M.; Novković, Đorđe ; Ćoćić, Aleksandar; Bukurov, M.; Lečić, Milan

(Isfahan Univ Technology, Isfahan, 2022)

TY  - JOUR
AU  - Burazer, Jela M.
AU  - Novković, Đorđe 
AU  - Ćoćić, Aleksandar
AU  - Bukurov, M.
AU  - Lečić, Milan
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3713
AB  - Vortex tube is a device without moving parts with ability to separate pressurized gas into two streams: cold and hot. This is a consequence of the Eckert-Wiese effect, which is responsible for spontaneous redistribution of total energy within the flow domain. In order for vortex tubes to work properly, there are some constraints which have to be fulfilled. The most important constraint in that sense is the L/D ratio. One part of this paper is dedicated to the research of the influence of L/D ratio on the energy separation in a vortex tube, i.e. to the values of total temperatures on cold and hot outlets of the device. On the other hand, experimental research of the inner flow is quite challenging since vortex tube is a device of small dimensions. Hence, we are relaying on numerical computations. One of important quantities that has to be prescribed in these computations is the turbulent Prandtl number Pr-T. Because of that, the other part of this paper is dedicated to research of the influence of Pr-T on the results of numerical computations. The research is conducted using open-source software OpenFOAM. Turbulence is modelled using two-equation and RST models. For small L/D ratios there is a secondary circulation that acts as a refrigeration cycle, and for greater L/D ratios distribution of velocity and temperature inside the vortex tube remains the same, regardless of the stagnation point presence. It is not justified to increase the length of the vortex tube beyond 20D since the change in cold total temperature inside the vortex tube as well at the cold outlet is practically null. For L/D variation from 1.8 to 10, the cold outlet temperature changes from 270.9 K to 266.8 K, and then rises to its final value of 270.5 K. For L/D ratio from 20 to 60, the total temperature at cold end remains unchanged at 271.3 K. We obtained good results with the unit value of turbulent Prandtl number, and demonstrated that increasing the Pr-T beyond unit value is not necessary in order to numerically obtain the energy separation inside the vortex tube.
PB  - Isfahan Univ Technology, Isfahan
T2  - Journal of Applied Fluid Mechanics
T1  - Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube
EP  - 1511
IS  - 5
SP  - 1503
VL  - 15
DO  - 10.47176/jafm.15.05.1168
ER  - 
@article{
author = "Burazer, Jela M. and Novković, Đorđe  and Ćoćić, Aleksandar and Bukurov, M. and Lečić, Milan",
year = "2022",
abstract = "Vortex tube is a device without moving parts with ability to separate pressurized gas into two streams: cold and hot. This is a consequence of the Eckert-Wiese effect, which is responsible for spontaneous redistribution of total energy within the flow domain. In order for vortex tubes to work properly, there are some constraints which have to be fulfilled. The most important constraint in that sense is the L/D ratio. One part of this paper is dedicated to the research of the influence of L/D ratio on the energy separation in a vortex tube, i.e. to the values of total temperatures on cold and hot outlets of the device. On the other hand, experimental research of the inner flow is quite challenging since vortex tube is a device of small dimensions. Hence, we are relaying on numerical computations. One of important quantities that has to be prescribed in these computations is the turbulent Prandtl number Pr-T. Because of that, the other part of this paper is dedicated to research of the influence of Pr-T on the results of numerical computations. The research is conducted using open-source software OpenFOAM. Turbulence is modelled using two-equation and RST models. For small L/D ratios there is a secondary circulation that acts as a refrigeration cycle, and for greater L/D ratios distribution of velocity and temperature inside the vortex tube remains the same, regardless of the stagnation point presence. It is not justified to increase the length of the vortex tube beyond 20D since the change in cold total temperature inside the vortex tube as well at the cold outlet is practically null. For L/D variation from 1.8 to 10, the cold outlet temperature changes from 270.9 K to 266.8 K, and then rises to its final value of 270.5 K. For L/D ratio from 20 to 60, the total temperature at cold end remains unchanged at 271.3 K. We obtained good results with the unit value of turbulent Prandtl number, and demonstrated that increasing the Pr-T beyond unit value is not necessary in order to numerically obtain the energy separation inside the vortex tube.",
publisher = "Isfahan Univ Technology, Isfahan",
journal = "Journal of Applied Fluid Mechanics",
title = "Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube",
pages = "1511-1503",
number = "5",
volume = "15",
doi = "10.47176/jafm.15.05.1168"
}
Burazer, J. M., Novković, Đ., Ćoćić, A., Bukurov, M.,& Lečić, M.. (2022). Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube. in Journal of Applied Fluid Mechanics
Isfahan Univ Technology, Isfahan., 15(5), 1503-1511.
https://doi.org/10.47176/jafm.15.05.1168
Burazer JM, Novković Đ, Ćoćić A, Bukurov M, Lečić M. Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube. in Journal of Applied Fluid Mechanics. 2022;15(5):1503-1511.
doi:10.47176/jafm.15.05.1168 .
Burazer, Jela M., Novković, Đorđe , Ćoćić, Aleksandar, Bukurov, M., Lečić, Milan, "Numerical Study of the L/D Ratio and Turbulent Prandtl Number Effect on Energy Separation in a Counter-Flow Vortex Tube" in Journal of Applied Fluid Mechanics, 15, no. 5 (2022):1503-1511,
https://doi.org/10.47176/jafm.15.05.1168 . .
1

Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control

Skoko, D. M.; Crnojević, C. D.; Lečić, Milan; Ristivojević, Mileta; Mitrović, Radivoje; Burazer, Jela M.

(Springer, New York, 2022)

TY  - JOUR
AU  - Skoko, D. M.
AU  - Crnojević, C. D.
AU  - Lečić, Milan
AU  - Ristivojević, Mileta
AU  - Mitrović, Radivoje
AU  - Burazer, Jela M.
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3733
AB  - The present paper studies the impingement of compressible air jet on a flat plate primarily from the aspect of its application in the domain of pneumatic metrology, i.e. in cases of small distance between the jet nozzle exit and the flat plate. Besides this direct application in the area of pneumatic metrology, the distance between the nozzle exit and the flat plate has been considerably increased and the case of a free jet was analysed with a view to compare the results applicable in various domains. This experimental study demonstrates that the structures of a free jet and this special case of an impingement jet are totally different. In the pressure distribution of the impingement jet, pressure discontinuity above the flat plate may occur, which is shown to be the result of low intensity shock waves and transonic flow. The experimental results show that the pneumatic sensitivity of a pneumatic comparator is a function of the supply pressure and the internal orifice diameter, as well as that the impingement air jet is a typical case of non-isentropic flow.
PB  - Springer, New York
T2  - Experimental Techniques
T1  - Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control
EP  - 113
IS  - 1
SP  - 103
VL  - 46
DO  - 10.1007/s40799-021-00460-6
ER  - 
@article{
author = "Skoko, D. M. and Crnojević, C. D. and Lečić, Milan and Ristivojević, Mileta and Mitrović, Radivoje and Burazer, Jela M.",
year = "2022",
abstract = "The present paper studies the impingement of compressible air jet on a flat plate primarily from the aspect of its application in the domain of pneumatic metrology, i.e. in cases of small distance between the jet nozzle exit and the flat plate. Besides this direct application in the area of pneumatic metrology, the distance between the nozzle exit and the flat plate has been considerably increased and the case of a free jet was analysed with a view to compare the results applicable in various domains. This experimental study demonstrates that the structures of a free jet and this special case of an impingement jet are totally different. In the pressure distribution of the impingement jet, pressure discontinuity above the flat plate may occur, which is shown to be the result of low intensity shock waves and transonic flow. The experimental results show that the pneumatic sensitivity of a pneumatic comparator is a function of the supply pressure and the internal orifice diameter, as well as that the impingement air jet is a typical case of non-isentropic flow.",
publisher = "Springer, New York",
journal = "Experimental Techniques",
title = "Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control",
pages = "113-103",
number = "1",
volume = "46",
doi = "10.1007/s40799-021-00460-6"
}
Skoko, D. M., Crnojević, C. D., Lečić, M., Ristivojević, M., Mitrović, R.,& Burazer, J. M.. (2022). Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control. in Experimental Techniques
Springer, New York., 46(1), 103-113.
https://doi.org/10.1007/s40799-021-00460-6
Skoko DM, Crnojević CD, Lečić M, Ristivojević M, Mitrović R, Burazer JM. Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control. in Experimental Techniques. 2022;46(1):103-113.
doi:10.1007/s40799-021-00460-6 .
Skoko, D. M., Crnojević, C. D., Lečić, Milan, Ristivojević, Mileta, Mitrović, Radivoje, Burazer, Jela M., "Some Characteristics of Compressible Air Impingement Jet Applied in Pneumatic Dimensional Control" in Experimental Techniques, 46, no. 1 (2022):103-113,
https://doi.org/10.1007/s40799-021-00460-6 . .
3
3

Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses

Čantrak, Đorđe; Janković, Novica; Nedeljković, Miloš

(WILEY, 2021)

TY  - CONF
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Nedeljković, Miloš
PY  - 2021
UR  - https://onlinelibrary.wiley.com/doi/10.1002/pamm.202000051
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6351
AB  - Kolmogorov has formulated his two hypotheses of similarity in 1941 considering local-isotropic turbulence, and later has
refined his theory [1, 2]. In this paper are discussed three turbulent swirl flows generated by the three various axial fan types
in-built in the pipe. The spectral characteristics of the generated turbulent swirl flows are determined on the basis on the LDA
(laser Doppler anemometry) experimental data for the circumferential velocity. In the inertial subranges these curves have the
same tangent and obey the “- 5/3” Kolmogorov law. It is shown that in the generated turbulent swirl flows occur eddies of
various scales, encompassing very wide spectra of wave numbers, i.e. frequencies.
PB  - WILEY
C3  - Proceedings in Applied Mathematics and Mechanics (PAMM)
T1  - Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses
VL  - 20
DO  - 10.1002/pamm.202000051
ER  - 
@conference{
author = "Čantrak, Đorđe and Janković, Novica and Nedeljković, Miloš",
year = "2021",
abstract = "Kolmogorov has formulated his two hypotheses of similarity in 1941 considering local-isotropic turbulence, and later has
refined his theory [1, 2]. In this paper are discussed three turbulent swirl flows generated by the three various axial fan types
in-built in the pipe. The spectral characteristics of the generated turbulent swirl flows are determined on the basis on the LDA
(laser Doppler anemometry) experimental data for the circumferential velocity. In the inertial subranges these curves have the
same tangent and obey the “- 5/3” Kolmogorov law. It is shown that in the generated turbulent swirl flows occur eddies of
various scales, encompassing very wide spectra of wave numbers, i.e. frequencies.",
publisher = "WILEY",
journal = "Proceedings in Applied Mathematics and Mechanics (PAMM)",
title = "Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses",
volume = "20",
doi = "10.1002/pamm.202000051"
}
Čantrak, Đ., Janković, N.,& Nedeljković, M.. (2021). Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses. in Proceedings in Applied Mathematics and Mechanics (PAMM)
WILEY., 20.
https://doi.org/10.1002/pamm.202000051
Čantrak Đ, Janković N, Nedeljković M. Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses. in Proceedings in Applied Mathematics and Mechanics (PAMM). 2021;20.
doi:10.1002/pamm.202000051 .
Čantrak, Đorđe, Janković, Novica, Nedeljković, Miloš, "Turbulent Swirl Flow Analysis by Kolmogorov’s Similarity Hypotheses" in Proceedings in Applied Mathematics and Mechanics (PAMM), 20 (2021),
https://doi.org/10.1002/pamm.202000051 . .
1

Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields

Bojović, Dušan; Čantrak, Đorđe; Janković, Novica; Nedeljković, Miloš

(Српско друштво за механику, 2021)

TY  - CONF
AU  - Bojović, Dušan
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Nedeljković, Miloš
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6343
AB  - In this paper is presented the Fast Response Aerodynamic Probe (FRAP), for measurements of the nonstationary fluid flow, widely present in the energy systems. Multihole probes are well known in experimental fluid mechanics. This is, on the contrary to the optical velocity measurement techniques, intrusive anemometry and pressure measuring device. It is, recently, updated with fast response sensors, which enable good sampling rate, necessary for turbulence study. 
Calibrations, aerodynamic, as well as dynamic one, and working principles of the FRAP probe are introduced. Probe design and implemented sensors are presented and described in numerous details.
Design of the test rig for necessary pitch-yaw aerodynamic calibration is developed and it is planned to achieve automated calibration procedure.
Results of the dynamic/acoustic calibration reveal fast probes response, up to 10 kHz.In addition, results of the first aerodynamic calibration for one velocity are presented and discussed. Obtained map of the calibration angles is provided, as well as diagrams of two out of five measured pressures. Determined velocity is, also, presented and analyzed error.
PB  - Српско друштво за механику
C3  - The 8th International Congress of Serbian Society of Mechanics
T1  - Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields
SP  - 557
UR  - https://hdl.handle.net/21.15107/rcub_machinery_6343
ER  - 
@conference{
author = "Bojović, Dušan and Čantrak, Đorđe and Janković, Novica and Nedeljković, Miloš",
year = "2021",
abstract = "In this paper is presented the Fast Response Aerodynamic Probe (FRAP), for measurements of the nonstationary fluid flow, widely present in the energy systems. Multihole probes are well known in experimental fluid mechanics. This is, on the contrary to the optical velocity measurement techniques, intrusive anemometry and pressure measuring device. It is, recently, updated with fast response sensors, which enable good sampling rate, necessary for turbulence study. 
Calibrations, aerodynamic, as well as dynamic one, and working principles of the FRAP probe are introduced. Probe design and implemented sensors are presented and described in numerous details.
Design of the test rig for necessary pitch-yaw aerodynamic calibration is developed and it is planned to achieve automated calibration procedure.
Results of the dynamic/acoustic calibration reveal fast probes response, up to 10 kHz.In addition, results of the first aerodynamic calibration for one velocity are presented and discussed. Obtained map of the calibration angles is provided, as well as diagrams of two out of five measured pressures. Determined velocity is, also, presented and analyzed error.",
publisher = "Српско друштво за механику",
journal = "The 8th International Congress of Serbian Society of Mechanics",
title = "Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields",
pages = "557",
url = "https://hdl.handle.net/21.15107/rcub_machinery_6343"
}
Bojović, D., Čantrak, Đ., Janković, N.,& Nedeljković, M.. (2021). Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields. in The 8th International Congress of Serbian Society of Mechanics
Српско друштво за механику., 557.
https://hdl.handle.net/21.15107/rcub_machinery_6343
Bojović D, Čantrak Đ, Janković N, Nedeljković M. Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields. in The 8th International Congress of Serbian Society of Mechanics. 2021;:557.
https://hdl.handle.net/21.15107/rcub_machinery_6343 .
Bojović, Dušan, Čantrak, Đorđe, Janković, Novica, Nedeljković, Miloš, "Five Hole Fast Response Probe for Measurements of 3D Velocity and Pressure Fields" in The 8th International Congress of Serbian Society of Mechanics (2021):557,
https://hdl.handle.net/21.15107/rcub_machinery_6343 .

Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries

Čantrak, Đorđe; Janković, Novica; Nedeljković, Miloš

(WILEY, 2021)

TY  - JOUR
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Nedeljković, Miloš
PY  - 2021
UR  - https://onlinelibrary.wiley.com/doi/10.1002/pamm.202100177
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6352
AB  - Kolmogorov has formulated his two hypotheses of similarity in 1941 considering local-isotropic turbulence, and later has
refined his theory [1, 2]. In this paper are discussed three turbulent swirl flows generated by the three various axial fan types
in-built in the pipe. The spectral characteristics of the generated turbulent swirl flows are determined on the basis on the LDA
(laser Doppler anemometry) experimental data for the circumferential velocity. In the inertial subranges these curves have the
same tangent and obey the “- 5/3” Kolmogorov law. It is shown that in the generated turbulent swirl flows occur eddies of
various scales, encompassing very wide spectra of wave numbers, i.e. frequencies.
PB  - WILEY
T2  - Proceedings in Applied Mathematics and Mechanics (PAMM)
T1  - Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries
VL  - 21
DO  - 10.1002/pamm.202100177
ER  - 
@article{
author = "Čantrak, Đorđe and Janković, Novica and Nedeljković, Miloš",
year = "2021",
abstract = "Kolmogorov has formulated his two hypotheses of similarity in 1941 considering local-isotropic turbulence, and later has
refined his theory [1, 2]. In this paper are discussed three turbulent swirl flows generated by the three various axial fan types
in-built in the pipe. The spectral characteristics of the generated turbulent swirl flows are determined on the basis on the LDA
(laser Doppler anemometry) experimental data for the circumferential velocity. In the inertial subranges these curves have the
same tangent and obey the “- 5/3” Kolmogorov law. It is shown that in the generated turbulent swirl flows occur eddies of
various scales, encompassing very wide spectra of wave numbers, i.e. frequencies.",
publisher = "WILEY",
journal = "Proceedings in Applied Mathematics and Mechanics (PAMM)",
title = "Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries",
volume = "21",
doi = "10.1002/pamm.202100177"
}
Čantrak, Đ., Janković, N.,& Nedeljković, M.. (2021). Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries. in Proceedings in Applied Mathematics and Mechanics (PAMM)
WILEY., 21.
https://doi.org/10.1002/pamm.202100177
Čantrak Đ, Janković N, Nedeljković M. Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries. in Proceedings in Applied Mathematics and Mechanics (PAMM). 2021;21.
doi:10.1002/pamm.202100177 .
Čantrak, Đorđe, Janković, Novica, Nedeljković, Miloš, "Kolmogorov's Similarity Hypotheses Application in Research of the Turbulent Swirl Flows in Pipe Generated by the Various Axial Fan Geometries" in Proceedings in Applied Mathematics and Mechanics (PAMM), 21 (2021),
https://doi.org/10.1002/pamm.202100177 . .

A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics

Ristić, Bogdan; Božić, Ivan; Simić, Aleksandar

(IOP Publishing Ltd, Bristol, 2021)

TY  - CONF
AU  - Ristić, Bogdan
AU  - Božić, Ivan
AU  - Simić, Aleksandar
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3613
AB  - It is sometimes economically unreasonable to develop specific turbines, but rather to use a well-known concept of a pump in the turbine mode - PAT (Pump As Turbine). Inspired by PAT, the scope of this paper covers the assessments of the possibility to use marine propellers as runners for the hydrokinetic turbines. Numerical analyses are conducted for selected propeller geometry with the aim of evaluating its energy characteristics in the turbine regime. The chosen propeller belongs to the conventional, thoroughly experimentally tested, Wageningen B -screw series. The experimental data were used for validation of the numerical results in propeller regimes. Based on the obtained results, the researched non-optimized turbine in its optimum regime achieves a satisfactory power coefficient which is close to the value of other types of contemporary hydrokinetic turbines efficiencies.
PB  - IOP Publishing Ltd, Bristol
C3  - 30th Iahr Symposium on Hydraulic Machinery and Systems (Iahr 2020)
T1  - A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics
VL  - 774
DO  - 10.1088/1755-1315/774/1/012063
ER  - 
@conference{
author = "Ristić, Bogdan and Božić, Ivan and Simić, Aleksandar",
year = "2021",
abstract = "It is sometimes economically unreasonable to develop specific turbines, but rather to use a well-known concept of a pump in the turbine mode - PAT (Pump As Turbine). Inspired by PAT, the scope of this paper covers the assessments of the possibility to use marine propellers as runners for the hydrokinetic turbines. Numerical analyses are conducted for selected propeller geometry with the aim of evaluating its energy characteristics in the turbine regime. The chosen propeller belongs to the conventional, thoroughly experimentally tested, Wageningen B -screw series. The experimental data were used for validation of the numerical results in propeller regimes. Based on the obtained results, the researched non-optimized turbine in its optimum regime achieves a satisfactory power coefficient which is close to the value of other types of contemporary hydrokinetic turbines efficiencies.",
publisher = "IOP Publishing Ltd, Bristol",
journal = "30th Iahr Symposium on Hydraulic Machinery and Systems (Iahr 2020)",
title = "A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics",
volume = "774",
doi = "10.1088/1755-1315/774/1/012063"
}
Ristić, B., Božić, I.,& Simić, A.. (2021). A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics. in 30th Iahr Symposium on Hydraulic Machinery and Systems (Iahr 2020)
IOP Publishing Ltd, Bristol., 774.
https://doi.org/10.1088/1755-1315/774/1/012063
Ristić B, Božić I, Simić A. A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics. in 30th Iahr Symposium on Hydraulic Machinery and Systems (Iahr 2020). 2021;774.
doi:10.1088/1755-1315/774/1/012063 .
Ristić, Bogdan, Božić, Ivan, Simić, Aleksandar, "A marine propeller as a hydrokinetic turbine - CFD analysis of energy characteristics" in 30th Iahr Symposium on Hydraulic Machinery and Systems (Iahr 2020), 774 (2021),
https://doi.org/10.1088/1755-1315/774/1/012063 . .
1
1

Modelling of three-dimensional particle rebound from an anisotropic rough wall

Radenković, Darko; Simonin, Olivier

(Elsevier, Amsterdam, 2021)

TY  - JOUR
AU  - Radenković, Darko
AU  - Simonin, Olivier
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3489
AB  - In gas-solid confined flows, particle rebound on a rough wall may have a great influence on the macroscopic properties of both phases. Existing simulation methods use simplified approaches where surface roughness is modelled as two-dimensional or isotropic. To improve the accuracy of such simulations, an anisotropic virtual rough wall statistical approach and the corresponding Lagrangian stochastic particle-wall collision model are proposed. From deterministic simulations of the impact of particles on the anisotropic virtual wall given as correlated bi-Gaussian surface, wall-normal vector angle statistics are used for model development. Rebound angle statistics computed from deterministic simulations and using the proposed stochastic model are in very good agreement. Incident particles in vertical planes not collinear with one of the principal directions of the anisotropic rough surface are bouncing with a mean transverse angle towards the principal direction of lower roughness.
PB  - Elsevier, Amsterdam
T2  - Powder Technology
T1  - Modelling of three-dimensional particle rebound from an anisotropic rough wall
EP  - 183
SP  - 165
VL  - 393
DO  - 10.1016/j.powtec.2021.07.055
ER  - 
@article{
author = "Radenković, Darko and Simonin, Olivier",
year = "2021",
abstract = "In gas-solid confined flows, particle rebound on a rough wall may have a great influence on the macroscopic properties of both phases. Existing simulation methods use simplified approaches where surface roughness is modelled as two-dimensional or isotropic. To improve the accuracy of such simulations, an anisotropic virtual rough wall statistical approach and the corresponding Lagrangian stochastic particle-wall collision model are proposed. From deterministic simulations of the impact of particles on the anisotropic virtual wall given as correlated bi-Gaussian surface, wall-normal vector angle statistics are used for model development. Rebound angle statistics computed from deterministic simulations and using the proposed stochastic model are in very good agreement. Incident particles in vertical planes not collinear with one of the principal directions of the anisotropic rough surface are bouncing with a mean transverse angle towards the principal direction of lower roughness.",
publisher = "Elsevier, Amsterdam",
journal = "Powder Technology",
title = "Modelling of three-dimensional particle rebound from an anisotropic rough wall",
pages = "183-165",
volume = "393",
doi = "10.1016/j.powtec.2021.07.055"
}
Radenković, D.,& Simonin, O.. (2021). Modelling of three-dimensional particle rebound from an anisotropic rough wall. in Powder Technology
Elsevier, Amsterdam., 393, 165-183.
https://doi.org/10.1016/j.powtec.2021.07.055
Radenković D, Simonin O. Modelling of three-dimensional particle rebound from an anisotropic rough wall. in Powder Technology. 2021;393:165-183.
doi:10.1016/j.powtec.2021.07.055 .
Radenković, Darko, Simonin, Olivier, "Modelling of three-dimensional particle rebound from an anisotropic rough wall" in Powder Technology, 393 (2021):165-183,
https://doi.org/10.1016/j.powtec.2021.07.055 . .
1
4
3

Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora

Janković, Novica

(Univerzitet u Beogradu, Mašinski fakultet, 2020)

TY  - THES
AU  - Janković, Novica
PY  - 2020
UR  - http://eteze.bg.ac.rs/application/showtheses?thesesId=8006
UR  - https://fedorabg.bg.ac.rs/fedora/get/o:23393/bdef:Content/download
UR  - http://vbs.rs/scripts/cobiss?command=DISPLAY&base=70036&RID=27898889
UR  - https://nardus.mpn.gov.rs/handle/123456789/18158
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/76
AB  - U okviru disertacije se istražuje struktura turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora. Generisano turbulentno strujanje je trodimenziono, nehomogeno i anizotropno. Primenjeni su složeni eksperimentalni, numerički i teorijski pristupi. Eksperimentalna instalacija je u radu detaljno opisana, kao i kvantifikacija merne nesigurnosti trokomponentnog sistema za Laser Dopler anemometriju (LDA). LDA sistem je, pri simultanom merenju tri komponente brzine, zahtevao precizna podešavanja merne zapremine u granicama prečnika do 100 μm. Ostvareno je precizno pomeranje ove zapremine duž mlaza. Poseban izazov je predstavljala numerička obrada dobijenih, u vremenu nejednako raspoređenih, mernih rezultata. Teorijskim razmatranjima, u okviru disertacije, bačeno je novo svetlo na klasične zapise Navije-Stoksovih i Rejnoldsovih jednačina u polarno-cilindričnim koordinatama. Detaljno su razmatrane empirijske radijalnoaksijalne raspodele ukupne, aksijalne, radijalne i obimske brzine, izmerene za dve brzine obrtanja ventilatora i tri ugla lopatica. Na ovaj način je bilo moguće istražiti uticaj Rejnoldsovog broja, kao i geometrijskih karakteristika ventilatora, tj. ugla lopatica, na karakter dejstva vihora na turbulenciju i evoluciju nivoa turbulencije, kako u samom mernom preseku, tako i u nizstrujnom razvoju mlaza. Analiza generisanja turbulencije i produkcije pojedinih Rejnoldsovih napona ukazala je na bitne karakteristike turbulentnog prenosa u slobodnom vihornom mlazu. Uočeno je da promena znaka gradijenta brzine ne izaziva uvek i promenu znaka pripadajuće komponente tenzora turbulentnog napona. U domenima strujnog polja u kojima se to dešava, mehanizam turbulentnog prenosa je nelokalnog karaktera, prisutna je negradijentna turbulentna difuzija i javlja se negativna produkcija kinetičke energije turbulencije. Izložena je diskusija o uticaju vihora na strukturu turbulencije i mehanizam turbulentnog prenosa. Analiza je ukazala na složena međudejstva osrednjenih i fluktuacionih polja u vihornom mlazu. Zaključeno je da generisanje energije fluktuacionog kretanja ne nastaje na osnovu kinetičke energije osrednjenog kretanja, već naprotiv. Smer prenošenja energije se menja, tako da osrednjeno kretanje „crpi” kinetičku energiju fluktuacionog kretanja, štoodgovara složenim strukturalnim svojstvima turbulencije. Zato su eksperimentalna istraživanja bila usmerena na merenje i analizu statističkih momenata višeg reda, i to ovde do šestog reda...
AB  - The dissertation deals with the structure of the turbulent swirl flow in an axial fan jet. The generated turbulent flow is three-dimensional, inhomogeneous and anisotropic. Complex experimental, numerical and theoretical approaches were applied. The experimental setup is described in detail, as well as the quantification of the measurement uncertainty of a three-component Laser Doppler Anemometry (LDA) system. The LDA system, while measuring the three velocity components simultaneously, requires precise adjustments of the measuring volume up to 100 μm in diameter. A precise displacement of this volume along the jet was achieved. A particular challenge was the numerical processing of the obtained unequally spaced data. Theoretical considerations, in the framework of the dissertation, have brought new light on classical notations of Navier-Stokes and Reynolds equations in polar-cylindrical coordinates. The empirical radial-axial distributions of total, axial, radial, and circumferential velocities measured for two fan speeds and three vanes angles are thoroughly analyzed. In this way, it was possible to investigate the influence of the Reynolds number as well as the geometric characteristics of the fan, i.e. angles of the blades, on the character of the swirl influence on turbulence and the evolution of the turbulence level, both in the measuring cross section and in the downstream development of the jet. An analysis of the generation of turbulence and the production of individual Reynolds stresses indicated the essential characteristics of turbulent transfer in a free swirl jet. It has been observed that a change in the sign of the velocity gradient does not always cause a change in the sign of the corresponding component of the turbulent stress tensor. In the fluid flow domains where this occurs, the turbulent transfer mechanism has nonlocal character, non-gradient turbulent diffusion and negative production of turbulence kinetic energy occur. Discussion of the effect of the swirl on the turbulence structure and the mechanism of turbulent transfer is presented. The analysis indicated the complex interactions of averaged and fluctuating fields in a swirl flow. It is concluded that the generation of fluctuating motion energy does not occur on the basis of kinetic energy of averaged motion, but on the contrary. The direction of energy transfer changes so that theaveraged motion "draws" the kinetic energy of the fluctuating motion, which corresponds to the complex structural properties of the turbulence. That is why experimental research has focused on measuring and analyzing higher order statistical moments, up to the sixth order here...
PB  - Univerzitet u Beogradu, Mašinski fakultet
T1  - Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora
T1  - Experimental and theoretical research of the structure of turbulent swirl flow in axial fan jet
UR  - https://hdl.handle.net/21.15107/rcub_nardus_18158
ER  - 
@phdthesis{
author = "Janković, Novica",
year = "2020",
abstract = "U okviru disertacije se istražuje struktura turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora. Generisano turbulentno strujanje je trodimenziono, nehomogeno i anizotropno. Primenjeni su složeni eksperimentalni, numerički i teorijski pristupi. Eksperimentalna instalacija je u radu detaljno opisana, kao i kvantifikacija merne nesigurnosti trokomponentnog sistema za Laser Dopler anemometriju (LDA). LDA sistem je, pri simultanom merenju tri komponente brzine, zahtevao precizna podešavanja merne zapremine u granicama prečnika do 100 μm. Ostvareno je precizno pomeranje ove zapremine duž mlaza. Poseban izazov je predstavljala numerička obrada dobijenih, u vremenu nejednako raspoređenih, mernih rezultata. Teorijskim razmatranjima, u okviru disertacije, bačeno je novo svetlo na klasične zapise Navije-Stoksovih i Rejnoldsovih jednačina u polarno-cilindričnim koordinatama. Detaljno su razmatrane empirijske radijalnoaksijalne raspodele ukupne, aksijalne, radijalne i obimske brzine, izmerene za dve brzine obrtanja ventilatora i tri ugla lopatica. Na ovaj način je bilo moguće istražiti uticaj Rejnoldsovog broja, kao i geometrijskih karakteristika ventilatora, tj. ugla lopatica, na karakter dejstva vihora na turbulenciju i evoluciju nivoa turbulencije, kako u samom mernom preseku, tako i u nizstrujnom razvoju mlaza. Analiza generisanja turbulencije i produkcije pojedinih Rejnoldsovih napona ukazala je na bitne karakteristike turbulentnog prenosa u slobodnom vihornom mlazu. Uočeno je da promena znaka gradijenta brzine ne izaziva uvek i promenu znaka pripadajuće komponente tenzora turbulentnog napona. U domenima strujnog polja u kojima se to dešava, mehanizam turbulentnog prenosa je nelokalnog karaktera, prisutna je negradijentna turbulentna difuzija i javlja se negativna produkcija kinetičke energije turbulencije. Izložena je diskusija o uticaju vihora na strukturu turbulencije i mehanizam turbulentnog prenosa. Analiza je ukazala na složena međudejstva osrednjenih i fluktuacionih polja u vihornom mlazu. Zaključeno je da generisanje energije fluktuacionog kretanja ne nastaje na osnovu kinetičke energije osrednjenog kretanja, već naprotiv. Smer prenošenja energije se menja, tako da osrednjeno kretanje „crpi” kinetičku energiju fluktuacionog kretanja, štoodgovara složenim strukturalnim svojstvima turbulencije. Zato su eksperimentalna istraživanja bila usmerena na merenje i analizu statističkih momenata višeg reda, i to ovde do šestog reda..., The dissertation deals with the structure of the turbulent swirl flow in an axial fan jet. The generated turbulent flow is three-dimensional, inhomogeneous and anisotropic. Complex experimental, numerical and theoretical approaches were applied. The experimental setup is described in detail, as well as the quantification of the measurement uncertainty of a three-component Laser Doppler Anemometry (LDA) system. The LDA system, while measuring the three velocity components simultaneously, requires precise adjustments of the measuring volume up to 100 μm in diameter. A precise displacement of this volume along the jet was achieved. A particular challenge was the numerical processing of the obtained unequally spaced data. Theoretical considerations, in the framework of the dissertation, have brought new light on classical notations of Navier-Stokes and Reynolds equations in polar-cylindrical coordinates. The empirical radial-axial distributions of total, axial, radial, and circumferential velocities measured for two fan speeds and three vanes angles are thoroughly analyzed. In this way, it was possible to investigate the influence of the Reynolds number as well as the geometric characteristics of the fan, i.e. angles of the blades, on the character of the swirl influence on turbulence and the evolution of the turbulence level, both in the measuring cross section and in the downstream development of the jet. An analysis of the generation of turbulence and the production of individual Reynolds stresses indicated the essential characteristics of turbulent transfer in a free swirl jet. It has been observed that a change in the sign of the velocity gradient does not always cause a change in the sign of the corresponding component of the turbulent stress tensor. In the fluid flow domains where this occurs, the turbulent transfer mechanism has nonlocal character, non-gradient turbulent diffusion and negative production of turbulence kinetic energy occur. Discussion of the effect of the swirl on the turbulence structure and the mechanism of turbulent transfer is presented. The analysis indicated the complex interactions of averaged and fluctuating fields in a swirl flow. It is concluded that the generation of fluctuating motion energy does not occur on the basis of kinetic energy of averaged motion, but on the contrary. The direction of energy transfer changes so that theaveraged motion "draws" the kinetic energy of the fluctuating motion, which corresponds to the complex structural properties of the turbulence. That is why experimental research has focused on measuring and analyzing higher order statistical moments, up to the sixth order here...",
publisher = "Univerzitet u Beogradu, Mašinski fakultet",
title = "Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora, Experimental and theoretical research of the structure of turbulent swirl flow in axial fan jet",
url = "https://hdl.handle.net/21.15107/rcub_nardus_18158"
}
Janković, N.. (2020). Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora. 
Univerzitet u Beogradu, Mašinski fakultet..
https://hdl.handle.net/21.15107/rcub_nardus_18158
Janković N. Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora. 2020;.
https://hdl.handle.net/21.15107/rcub_nardus_18158 .
Janković, Novica, "Eksperimentalna i teorijska istraživanja strukture turbulentnog vihornog strujanja u mlazu aksijalnog ventilatora" (2020),
https://hdl.handle.net/21.15107/rcub_nardus_18158 .

Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration

Janković, Novica; Jeremić, Đorđe; Čantrak, Đorđe; Ilić, Dejan

(2020)

TY  - CONF
AU  - Janković, Novica
AU  - Jeremić, Đorđe
AU  - Čantrak, Đorđe
AU  - Ilić, Dejan
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5261
AB  - Existing wind tunnel in the Laboratory for Hydraulic machinery and energy systems, Faculty of Mechanical Engineering, University of Belgrade, is redesigned, by adding axial fan regulated by the inverter at the tunnel inlet and flow straightener in the pipe before the carefully profiled Witoshinsky nozzle. Various anemometers could be calibrated in the axisymmetric uniform jet after the nozzle with inner diameter of 145 mm. In this paper are presented experimental results of the flow uniformity and turbulence levels, as well as skewness and flatness distributions for various flow regimes in the wind tunnel measurement section by one-component laser Doppler anemometry (LDA) along the horizontal radius in 27 points. Time-averaged axial velocity profiles have been obtained for twenty Reynolds numbers in the interval Re = 1780 to 148869, determined for point on the jet axis r/R =0. Uniform velocity profiles are obtained in the jet core region, i.e. up to r/R = 0,9 for all Reynolds numbers except the lowest one. Turbulence levels have been also reported for all these cases and achieved turbulence levels were below 2% in the free jet core region for almost all measuring points and regimes, what follows standard ISO 17713-1 requirements. Achieved validation was high. Sampling rate varied and in most of the cases was in average 250-400 Hz. Thermal fog seeding was applied at the calibration tunnel inlet, i.e. at the axial fan suction side.
C3  - Proceedings, 9th International Scientific Conference on Defensive Technologies, OTEH 2020, Belgrade, Serbia, 15-16 October 2020., Session Quality, Standardization, Metrology, Maintenance and Exploitation, 6 pages, paper no. 013.
T1  - Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration
UR  - https://hdl.handle.net/21.15107/rcub_machinery_5261
ER  - 
@conference{
author = "Janković, Novica and Jeremić, Đorđe and Čantrak, Đorđe and Ilić, Dejan",
year = "2020",
abstract = "Existing wind tunnel in the Laboratory for Hydraulic machinery and energy systems, Faculty of Mechanical Engineering, University of Belgrade, is redesigned, by adding axial fan regulated by the inverter at the tunnel inlet and flow straightener in the pipe before the carefully profiled Witoshinsky nozzle. Various anemometers could be calibrated in the axisymmetric uniform jet after the nozzle with inner diameter of 145 mm. In this paper are presented experimental results of the flow uniformity and turbulence levels, as well as skewness and flatness distributions for various flow regimes in the wind tunnel measurement section by one-component laser Doppler anemometry (LDA) along the horizontal radius in 27 points. Time-averaged axial velocity profiles have been obtained for twenty Reynolds numbers in the interval Re = 1780 to 148869, determined for point on the jet axis r/R =0. Uniform velocity profiles are obtained in the jet core region, i.e. up to r/R = 0,9 for all Reynolds numbers except the lowest one. Turbulence levels have been also reported for all these cases and achieved turbulence levels were below 2% in the free jet core region for almost all measuring points and regimes, what follows standard ISO 17713-1 requirements. Achieved validation was high. Sampling rate varied and in most of the cases was in average 250-400 Hz. Thermal fog seeding was applied at the calibration tunnel inlet, i.e. at the axial fan suction side.",
journal = "Proceedings, 9th International Scientific Conference on Defensive Technologies, OTEH 2020, Belgrade, Serbia, 15-16 October 2020., Session Quality, Standardization, Metrology, Maintenance and Exploitation, 6 pages, paper no. 013.",
title = "Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration",
url = "https://hdl.handle.net/21.15107/rcub_machinery_5261"
}
Janković, N., Jeremić, Đ., Čantrak, Đ.,& Ilić, D.. (2020). Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration. in Proceedings, 9th International Scientific Conference on Defensive Technologies, OTEH 2020, Belgrade, Serbia, 15-16 October 2020., Session Quality, Standardization, Metrology, Maintenance and Exploitation, 6 pages, paper no. 013..
https://hdl.handle.net/21.15107/rcub_machinery_5261
Janković N, Jeremić Đ, Čantrak Đ, Ilić D. Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration. in Proceedings, 9th International Scientific Conference on Defensive Technologies, OTEH 2020, Belgrade, Serbia, 15-16 October 2020., Session Quality, Standardization, Metrology, Maintenance and Exploitation, 6 pages, paper no. 013.. 2020;.
https://hdl.handle.net/21.15107/rcub_machinery_5261 .
Janković, Novica, Jeremić, Đorđe, Čantrak, Đorđe, Ilić, Dejan, "Flow Uniformity and Turbulence Level Measurements by LDA in the Wind Tunnel for Anemometers Calibration" in Proceedings, 9th International Scientific Conference on Defensive Technologies, OTEH 2020, Belgrade, Serbia, 15-16 October 2020., Session Quality, Standardization, Metrology, Maintenance and Exploitation, 6 pages, paper no. 013. (2020),
https://hdl.handle.net/21.15107/rcub_machinery_5261 .

Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side

Čantrak, Đorđe; Janković, Novica; Ilić, Dejan

(2020)

TY  - CONF
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Ilić, Dejan
PY  - 2020
UR  - http://cnntechno.com/docs/4_CNN_book_of_abstracts_CIP_Final.pdf
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/5571
AB  - Some aspects of the laser Doppler anemometry (LDA) investigation of the turbulent swirl flow behind axial
fans in pipes, diffusers and jets are presented in this paper. All three installations have profiled bell mouth inlet,
while the fans are built-in in different ways. Namely, in the first case axial fan is built-in into the pipe
approximately 27.74D long, where D is average inner diameter D = 0.4 m. In the second case axial fan is builtin
into the straight conical diffuser with the inlet diameter 0.4 m and total divergence angle 8.6⁰, while in the
third case turbulent swirl jet flow behind the axial was observed. In all cases fan impeller rotation number is
varied. One-, as well as, two- and thee-component LDA systems were applied. Thermal fog seeding was
applied in all cases. Time averaged velocity profiles are analysed, as well as the statistical moments of the
second till the fourth order. In addition, distributions of the Reynolds stresses are also presented and
discussed. Investigations reveal structures, as well as complexity of the three-dimensional, non-homogenous,
anisotropic turbulent swirl flows. This stochastic character on the instantaneous level was shown for all three
cases. Kolmogorov “-5/3 law” is shown in the case of the circumferential velocity distribution for the turbulent
swirl flow in the pipe for various measuring points. Phenomenon of the non-local turbulent transfer and nongradient
turbulent diffusion is studied. The influence of the axial fan duty point on the generated turbulence
structure is studied.
C3  - International Conference of Experimental and Numerical Investigations and New Technolgies, CNN TECH 2020, Session: Clear sky, June 29-July 2, Zlatibor, Serbia, pp. 65
T1  - Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side
SP  - 65
UR  - https://hdl.handle.net/21.15107/rcub_machinery_5571
ER  - 
@conference{
author = "Čantrak, Đorđe and Janković, Novica and Ilić, Dejan",
year = "2020",
abstract = "Some aspects of the laser Doppler anemometry (LDA) investigation of the turbulent swirl flow behind axial
fans in pipes, diffusers and jets are presented in this paper. All three installations have profiled bell mouth inlet,
while the fans are built-in in different ways. Namely, in the first case axial fan is built-in into the pipe
approximately 27.74D long, where D is average inner diameter D = 0.4 m. In the second case axial fan is builtin
into the straight conical diffuser with the inlet diameter 0.4 m and total divergence angle 8.6⁰, while in the
third case turbulent swirl jet flow behind the axial was observed. In all cases fan impeller rotation number is
varied. One-, as well as, two- and thee-component LDA systems were applied. Thermal fog seeding was
applied in all cases. Time averaged velocity profiles are analysed, as well as the statistical moments of the
second till the fourth order. In addition, distributions of the Reynolds stresses are also presented and
discussed. Investigations reveal structures, as well as complexity of the three-dimensional, non-homogenous,
anisotropic turbulent swirl flows. This stochastic character on the instantaneous level was shown for all three
cases. Kolmogorov “-5/3 law” is shown in the case of the circumferential velocity distribution for the turbulent
swirl flow in the pipe for various measuring points. Phenomenon of the non-local turbulent transfer and nongradient
turbulent diffusion is studied. The influence of the axial fan duty point on the generated turbulence
structure is studied.",
journal = "International Conference of Experimental and Numerical Investigations and New Technolgies, CNN TECH 2020, Session: Clear sky, June 29-July 2, Zlatibor, Serbia, pp. 65",
title = "Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side",
pages = "65",
url = "https://hdl.handle.net/21.15107/rcub_machinery_5571"
}
Čantrak, Đ., Janković, N.,& Ilić, D.. (2020). Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side. in International Conference of Experimental and Numerical Investigations and New Technolgies, CNN TECH 2020, Session: Clear sky, June 29-July 2, Zlatibor, Serbia, pp. 65, 65.
https://hdl.handle.net/21.15107/rcub_machinery_5571
Čantrak Đ, Janković N, Ilić D. Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side. in International Conference of Experimental and Numerical Investigations and New Technolgies, CNN TECH 2020, Session: Clear sky, June 29-July 2, Zlatibor, Serbia, pp. 65. 2020;:65.
https://hdl.handle.net/21.15107/rcub_machinery_5571 .
Čantrak, Đorđe, Janković, Novica, Ilić, Dejan, "Observations from LDA Research of the Turbulent Swirl Flow on the Axial Fan Pressure Side" in International Conference of Experimental and Numerical Investigations and New Technolgies, CNN TECH 2020, Session: Clear sky, June 29-July 2, Zlatibor, Serbia, pp. 65 (2020):65,
https://hdl.handle.net/21.15107/rcub_machinery_5571 .

New Design of the Reversible Jet Fan

Benišek, Miroslav; Čantrak, Đorđe; Ilić, Dejan; Janković, Novica

(MDPI, Basel, 2020)

TY  - JOUR
AU  - Benišek, Miroslav
AU  - Čantrak, Đorđe
AU  - Ilić, Dejan
AU  - Janković, Novica
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3340
AB  - This paper presents two designs of the axial reversible jet fan, with the special focus on the impeller. The intention was to develop a reversible axial jet fan which operates in the same way in both rotating directions while generating thrust as high as possible. The jet fan model with the outer diameter 499.2 +/- 0.1 mm and ten adjustable blades is the same, while it is in-built in two different casings. The first construction is a cylindrical casing, while the second one is profiled as a nozzle. Thrust, volume flow rate, consumed power and ambient conditions were measured after the international standard ISO 13350. Results for both constructions are presented for three impeller blade angles: 28 degrees, 31 degrees and 35 degrees, and rotation speed in the interval n = 400 to 2600 rpm. The smallest differences in thrust, depending on the fan rotation direction, as well as the highest thrust are achieved for the first design with the cylindrical casing and blade angle at the outer diameter of 35 degrees. Therefore, it was shown that fan casing significantly influences jet fan characteristics. In addition, the maximum thrust value and its independence of the flow direction is experimentally obtained for the angle of 39 degrees in the cylindrical casing.
PB  - MDPI, Basel
T2  - Processes
T1  - New Design of the Reversible Jet Fan
IS  - 12
VL  - 8
DO  - 10.3390/pr8121671
ER  - 
@article{
author = "Benišek, Miroslav and Čantrak, Đorđe and Ilić, Dejan and Janković, Novica",
year = "2020",
abstract = "This paper presents two designs of the axial reversible jet fan, with the special focus on the impeller. The intention was to develop a reversible axial jet fan which operates in the same way in both rotating directions while generating thrust as high as possible. The jet fan model with the outer diameter 499.2 +/- 0.1 mm and ten adjustable blades is the same, while it is in-built in two different casings. The first construction is a cylindrical casing, while the second one is profiled as a nozzle. Thrust, volume flow rate, consumed power and ambient conditions were measured after the international standard ISO 13350. Results for both constructions are presented for three impeller blade angles: 28 degrees, 31 degrees and 35 degrees, and rotation speed in the interval n = 400 to 2600 rpm. The smallest differences in thrust, depending on the fan rotation direction, as well as the highest thrust are achieved for the first design with the cylindrical casing and blade angle at the outer diameter of 35 degrees. Therefore, it was shown that fan casing significantly influences jet fan characteristics. In addition, the maximum thrust value and its independence of the flow direction is experimentally obtained for the angle of 39 degrees in the cylindrical casing.",
publisher = "MDPI, Basel",
journal = "Processes",
title = "New Design of the Reversible Jet Fan",
number = "12",
volume = "8",
doi = "10.3390/pr8121671"
}
Benišek, M., Čantrak, Đ., Ilić, D.,& Janković, N.. (2020). New Design of the Reversible Jet Fan. in Processes
MDPI, Basel., 8(12).
https://doi.org/10.3390/pr8121671
Benišek M, Čantrak Đ, Ilić D, Janković N. New Design of the Reversible Jet Fan. in Processes. 2020;8(12).
doi:10.3390/pr8121671 .
Benišek, Miroslav, Čantrak, Đorđe, Ilić, Dejan, Janković, Novica, "New Design of the Reversible Jet Fan" in Processes, 8, no. 12 (2020),
https://doi.org/10.3390/pr8121671 . .
4
3

Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education

Matijević, Milan S.; Nedeljković, Miloš

(Springer International Publishing Ag, Cham, 2020)

TY  - CONF
AU  - Matijević, Milan S.
AU  - Nedeljković, Miloš
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3320
AB  - This paper describes some pedagogical approaches of using electrical motors within engineering study programs. We are discussing the education of students who are without any electrical engineering background, and who only aim to use motors within different engineering applications like robots, hydro-mechanical or control engineering application. Laboratory support is typically expensive, especially for countries like Serbia, but laboratories are necessary for engineering education. The paper promotes problem-based learning approach which is based on affordable or as cheap as possible laboratory experiments.
PB  - Springer International Publishing Ag, Cham
C3  - Challenges of The Digital Transformation in Education, Icl2018, Vol 1
T1  - Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education
EP  - 844
SP  - 833
VL  - 916
DO  - 10.1007/978-3-030-11932-4_77
ER  - 
@conference{
author = "Matijević, Milan S. and Nedeljković, Miloš",
year = "2020",
abstract = "This paper describes some pedagogical approaches of using electrical motors within engineering study programs. We are discussing the education of students who are without any electrical engineering background, and who only aim to use motors within different engineering applications like robots, hydro-mechanical or control engineering application. Laboratory support is typically expensive, especially for countries like Serbia, but laboratories are necessary for engineering education. The paper promotes problem-based learning approach which is based on affordable or as cheap as possible laboratory experiments.",
publisher = "Springer International Publishing Ag, Cham",
journal = "Challenges of The Digital Transformation in Education, Icl2018, Vol 1",
title = "Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education",
pages = "844-833",
volume = "916",
doi = "10.1007/978-3-030-11932-4_77"
}
Matijević, M. S.,& Nedeljković, M.. (2020). Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education. in Challenges of The Digital Transformation in Education, Icl2018, Vol 1
Springer International Publishing Ag, Cham., 916, 833-844.
https://doi.org/10.1007/978-3-030-11932-4_77
Matijević MS, Nedeljković M. Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education. in Challenges of The Digital Transformation in Education, Icl2018, Vol 1. 2020;916:833-844.
doi:10.1007/978-3-030-11932-4_77 .
Matijević, Milan S., Nedeljković, Miloš, "Design and Use of Digitally Controlled Electric Motors for Purpose of Engineering Education" in Challenges of The Digital Transformation in Education, Icl2018, Vol 1, 916 (2020):833-844,
https://doi.org/10.1007/978-3-030-11932-4_77 . .

Pressure distribution in microtubes with variable cross section

Guranov, Iva; Milićev, Snežana; Stevanović, Nevena

(Serbian Society of Mechanics, 2019)

TY  - CONF
AU  - Guranov, Iva
AU  - Milićev, Snežana
AU  - Stevanović, Nevena
PY  - 2019
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3973
AB  - A steady compressible isothermal slip gas flow in a microtube is analyzed for low Reynolds 
numbers. The microtube is with varying cross-section, which from the standpoint of geometry 
gives three considered cases: convergent microtube, divergent microtube and microtube with 
constant radius. The gas flow is caused by the pressure difference between the inlet and the outlet 
cross-section. The solution for pressure and mass flow rate is obtained by macroscopic approach 
from Navier-Stokes equations with the second order velocity slip boundary condition. Analysis of 
the order of dimensionless terms in governing equations is possible with the usage of exact 
relation between Reynolds, Mach and Knudsen numbers. The solution procedure for this flow 
model is based on perturbation approach, where significant variables are assumed in the form of 
perturbation series. The first approximation represents the solution for the continuum flow 
conditions, and the second approximation incorporates the effect of gas rarefaction. The obtained 
solution is compared with verified results of numerical experiment found in literature and good 
agreement is achieved. Hence, the reliability of obtained solution and presented method is 
confirmed.
PB  - Serbian Society of Mechanics
C3  - Proceedings of the The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, June 24-26, 2019
T1  - Pressure distribution in microtubes with variable cross section
EP  - 8
SP  - 1
UR  - https://hdl.handle.net/21.15107/rcub_machinery_3973
ER  - 
@conference{
author = "Guranov, Iva and Milićev, Snežana and Stevanović, Nevena",
year = "2019",
abstract = "A steady compressible isothermal slip gas flow in a microtube is analyzed for low Reynolds 
numbers. The microtube is with varying cross-section, which from the standpoint of geometry 
gives three considered cases: convergent microtube, divergent microtube and microtube with 
constant radius. The gas flow is caused by the pressure difference between the inlet and the outlet 
cross-section. The solution for pressure and mass flow rate is obtained by macroscopic approach 
from Navier-Stokes equations with the second order velocity slip boundary condition. Analysis of 
the order of dimensionless terms in governing equations is possible with the usage of exact 
relation between Reynolds, Mach and Knudsen numbers. The solution procedure for this flow 
model is based on perturbation approach, where significant variables are assumed in the form of 
perturbation series. The first approximation represents the solution for the continuum flow 
conditions, and the second approximation incorporates the effect of gas rarefaction. The obtained 
solution is compared with verified results of numerical experiment found in literature and good 
agreement is achieved. Hence, the reliability of obtained solution and presented method is 
confirmed.",
publisher = "Serbian Society of Mechanics",
journal = "Proceedings of the The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, June 24-26, 2019",
title = "Pressure distribution in microtubes with variable cross section",
pages = "8-1",
url = "https://hdl.handle.net/21.15107/rcub_machinery_3973"
}
Guranov, I., Milićev, S.,& Stevanović, N.. (2019). Pressure distribution in microtubes with variable cross section. in Proceedings of the The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, June 24-26, 2019
Serbian Society of Mechanics., 1-8.
https://hdl.handle.net/21.15107/rcub_machinery_3973
Guranov I, Milićev S, Stevanović N. Pressure distribution in microtubes with variable cross section. in Proceedings of the The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, June 24-26, 2019. 2019;:1-8.
https://hdl.handle.net/21.15107/rcub_machinery_3973 .
Guranov, Iva, Milićev, Snežana, Stevanović, Nevena, "Pressure distribution in microtubes with variable cross section" in Proceedings of the The 7th International Congress of Serbian Society of Mechanics, Sremski Karlovci, June 24-26, 2019 (2019):1-8,
https://hdl.handle.net/21.15107/rcub_machinery_3973 .

Lectures in Rotodynamic Pumps - from Design and Simulations to Testing

Čantrak, Đorđe; Janković, Novica; Nedeljković, Miloš; Matijević, Milan S.; Ilić, Dejan

(Springer International Publishing Ag, Cham, 2019)

TY  - CONF
AU  - Čantrak, Đorđe
AU  - Janković, Novica
AU  - Nedeljković, Miloš
AU  - Matijević, Milan S.
AU  - Ilić, Dejan
PY  - 2019
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3008
AB  - Teaching in hydraulic machines at the University of Belgrade, Faculty of Mechanical Engineering, Chair for Hydraulic Machinery and Energy Systems has a long tradition starting back in the nineteenth century. Numerous experimental test rigs are designed and novel measurement techniques are applied. Students have an ability to design, perform computational fluid dynamics (CFD), manufacture, and test pump units with the supervision of lecturers. This practical work, with concept "do it yourself", attracts students to develop their abilities in 3D geometry modeling, computational fluid dynamics, computer-aided manufacturing (CAM), and application of novel acquisition and data processing softwares. Parallel to this, they develop a piping system, which will be coupled with the assembled centrifugal pump and run the first test. Afterward, they are stimulated to connect the acquisition system with LabView software. They are supported to develop their own application for pump and hydraulic components testing and to perform the tests. The final stage is to integrate this installation in Go-Lab Sharing platform repository or at the Hydraulic machinery and Energy Systems Department website. The purpose of this educational approach is to have well educated students, not only with good theoretical background, but also with practical skills and engineering way of thinking. They have to be able to develop the operational pump hydraulic system, and not only a component.
PB  - Springer International Publishing Ag, Cham
C3  - Proceedings / 2018 International Conference on Interactive Mobile Communication, Technologies and Learning (IMCL2018), McMaster University, Hamilton, Ontario, Canada, October 11-13
T1  - Lectures in Rotodynamic Pumps - from Design and Simulations to Testing
EP  - 406
SP  - 394
VL  - 909
DO  - 10.1007/978-3-030-11434-3_42
ER  - 
@conference{
author = "Čantrak, Đorđe and Janković, Novica and Nedeljković, Miloš and Matijević, Milan S. and Ilić, Dejan",
year = "2019",
abstract = "Teaching in hydraulic machines at the University of Belgrade, Faculty of Mechanical Engineering, Chair for Hydraulic Machinery and Energy Systems has a long tradition starting back in the nineteenth century. Numerous experimental test rigs are designed and novel measurement techniques are applied. Students have an ability to design, perform computational fluid dynamics (CFD), manufacture, and test pump units with the supervision of lecturers. This practical work, with concept "do it yourself", attracts students to develop their abilities in 3D geometry modeling, computational fluid dynamics, computer-aided manufacturing (CAM), and application of novel acquisition and data processing softwares. Parallel to this, they develop a piping system, which will be coupled with the assembled centrifugal pump and run the first test. Afterward, they are stimulated to connect the acquisition system with LabView software. They are supported to develop their own application for pump and hydraulic components testing and to perform the tests. The final stage is to integrate this installation in Go-Lab Sharing platform repository or at the Hydraulic machinery and Energy Systems Department website. The purpose of this educational approach is to have well educated students, not only with good theoretical background, but also with practical skills and engineering way of thinking. They have to be able to develop the operational pump hydraulic system, and not only a component.",
publisher = "Springer International Publishing Ag, Cham",
journal = "Proceedings / 2018 International Conference on Interactive Mobile Communication, Technologies and Learning (IMCL2018), McMaster University, Hamilton, Ontario, Canada, October 11-13",
title = "Lectures in Rotodynamic Pumps - from Design and Simulations to Testing",
pages = "406-394",
volume = "909",
doi = "10.1007/978-3-030-11434-3_42"
}
Čantrak, Đ., Janković, N., Nedeljković, M., Matijević, M. S.,& Ilić, D.. (2019). Lectures in Rotodynamic Pumps - from Design and Simulations to Testing. in Proceedings / 2018 International Conference on Interactive Mobile Communication, Technologies and Learning (IMCL2018), McMaster University, Hamilton, Ontario, Canada, October 11-13
Springer International Publishing Ag, Cham., 909, 394-406.
https://doi.org/10.1007/978-3-030-11434-3_42
Čantrak Đ, Janković N, Nedeljković M, Matijević MS, Ilić D. Lectures in Rotodynamic Pumps - from Design and Simulations to Testing. in Proceedings / 2018 International Conference on Interactive Mobile Communication, Technologies and Learning (IMCL2018), McMaster University, Hamilton, Ontario, Canada, October 11-13. 2019;909:394-406.
doi:10.1007/978-3-030-11434-3_42 .
Čantrak, Đorđe, Janković, Novica, Nedeljković, Miloš, Matijević, Milan S., Ilić, Dejan, "Lectures in Rotodynamic Pumps - from Design and Simulations to Testing" in Proceedings / 2018 International Conference on Interactive Mobile Communication, Technologies and Learning (IMCL2018), McMaster University, Hamilton, Ontario, Canada, October 11-13, 909 (2019):394-406,
https://doi.org/10.1007/978-3-030-11434-3_42 . .