Kolarević, Nenad

Link to this page

Authority KeyName Variants
orcid::0000-0003-2836-7405
  • Kolarević, Nenad (29)
Projects
Ministry of Education, Science and Technological Development, Republic of Serbia, Grant no. 200105 (University of Belgrade, Faculty of Mechanical Engineering) Pressure equipment integrity under simultaneous effect of fatigue loading and temperature
Development of the tribological micro/nano two component and hybrid selflubricating composites company EDePro - Engine Design and Production from Belgrade
Advanced multicomponent metal systems and nanostructured materials with diverse functional properties Low cost space transportation systems
National Nature Science Foundation of China [51950410600] company EDePro - Engine Design and Production from Belgrade, Serbia
company EDePro - Engine Design and Production in Belgrade Ministry of Education, Science and Technological Development, Republic of Serbia, Grant no. 200131 (University of Belgrade, Technical Faculty, Bor)
Ministry of Education, Science and Technological Development, Republic of Serbia, Grant no. 200135 (University of Belgrade, Faculty of Technology and Metallurgy) Ministry of Education, Science and Technological Development, Republic of Serbia, Grant no. 200155 (University of Priština - Kosovska Mitrovica, Faculty of Technical Science)
Ministry of Education, Science and Technological Development, Republic of Serbia, Grant no. 200213 (Innovation Center of the Faculty of Mechanical Engineering) Tests were performed in EDePro d.o.o. facilities in Belgrade as a part of UAV tip-jet helicopter development program.
The authors wish to acknowledge and thank the company EDePro - Engine Design and Production in Belgrade for support and for encouragement in the project realization.

Author's Bibliography

Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears

Stanković, Miloš; Mihajlović, Dimitrije; Kolarević, Nenad; Dimić, Aleksandar; Davidović, Nikola

(2023)

TY  - CONF
AU  - Stanković, Miloš
AU  - Mihajlović, Dimitrije
AU  - Kolarević, Nenad
AU  - Dimić, Aleksandar
AU  - Davidović, Nikola
PY  - 2023
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7640
C3  - 39th Danubia-Adria Symposium on Advances in Experimental Mechanics 26-29 September 2023
T1  - Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears
EP  - 33
SP  - 32
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7640
ER  - 
@conference{
author = "Stanković, Miloš and Mihajlović, Dimitrije and Kolarević, Nenad and Dimić, Aleksandar and Davidović, Nikola",
year = "2023",
journal = "39th Danubia-Adria Symposium on Advances in Experimental Mechanics 26-29 September 2023",
title = "Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears",
pages = "33-32",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7640"
}
Stanković, M., Mihajlović, D., Kolarević, N., Dimić, A.,& Davidović, N.. (2023). Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears. in 39th Danubia-Adria Symposium on Advances in Experimental Mechanics 26-29 September 2023, 32-33.
https://hdl.handle.net/21.15107/rcub_machinery_7640
Stanković M, Mihajlović D, Kolarević N, Dimić A, Davidović N. Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears. in 39th Danubia-Adria Symposium on Advances in Experimental Mechanics 26-29 September 2023. 2023;:32-33.
https://hdl.handle.net/21.15107/rcub_machinery_7640 .
Stanković, Miloš, Mihajlović, Dimitrije, Kolarević, Nenad, Dimić, Aleksandar, Davidović, Nikola, "Influence Of The Production Steps Onto The Teeth Geometry Of High Precision Gears" in 39th Danubia-Adria Symposium on Advances in Experimental Mechanics 26-29 September 2023 (2023):32-33,
https://hdl.handle.net/21.15107/rcub_machinery_7640 .

Influence Of Elastic Bearing Support on Labirinth Seal Operation

Kolarević, Nenad; Stanković, Miloš; Mihajlović, Dimitrije; Davidović, Nikola; Miloš, Marko

(2022)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Mihajlović, Dimitrije
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7637
C3  - 38th Danubia-Adria Symposium on Advances in Experimental Mechanics, 20-23 September 2022, Poros, Greece
T1  - Influence Of Elastic Bearing Support on Labirinth Seal Operation
EP  - 2
SP  - 1
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7637
ER  - 
@conference{
author = "Kolarević, Nenad and Stanković, Miloš and Mihajlović, Dimitrije and Davidović, Nikola and Miloš, Marko",
year = "2022",
journal = "38th Danubia-Adria Symposium on Advances in Experimental Mechanics, 20-23 September 2022, Poros, Greece",
title = "Influence Of Elastic Bearing Support on Labirinth Seal Operation",
pages = "2-1",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7637"
}
Kolarević, N., Stanković, M., Mihajlović, D., Davidović, N.,& Miloš, M.. (2022). Influence Of Elastic Bearing Support on Labirinth Seal Operation. in 38th Danubia-Adria Symposium on Advances in Experimental Mechanics, 20-23 September 2022, Poros, Greece, 1-2.
https://hdl.handle.net/21.15107/rcub_machinery_7637
Kolarević N, Stanković M, Mihajlović D, Davidović N, Miloš M. Influence Of Elastic Bearing Support on Labirinth Seal Operation. in 38th Danubia-Adria Symposium on Advances in Experimental Mechanics, 20-23 September 2022, Poros, Greece. 2022;:1-2.
https://hdl.handle.net/21.15107/rcub_machinery_7637 .
Kolarević, Nenad, Stanković, Miloš, Mihajlović, Dimitrije, Davidović, Nikola, Miloš, Marko, "Influence Of Elastic Bearing Support on Labirinth Seal Operation" in 38th Danubia-Adria Symposium on Advances in Experimental Mechanics, 20-23 September 2022, Poros, Greece (2022):1-2,
https://hdl.handle.net/21.15107/rcub_machinery_7637 .

Sealing of the High Speed Bearing Assemblies with One Elastic Support

Stanković, Miloš; Kolarević, Nenad; Mihajlović, Dimitrije; Ognjanović, Milosav; Davidović, Nikola; Miloš, Marko

(2022)

TY  - CONF
AU  - Stanković, Miloš
AU  - Kolarević, Nenad
AU  - Mihajlović, Dimitrije
AU  - Ognjanović, Milosav
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7639
AB  - High speed bearing assemblies are widely applied in many industries, especially in the airspace and automotive. Design of these assemblies is highly challenging due to some opposed factors affecting their proper functionality. On the one side, there is a condition of rotor-dynamics, which implies the shaft to rotate as stable as possible, retaining its original shape. In regards to this, it was observed that having one elastic and one stiff support, rather than having two stiff supports, provides better dynamic behaviour. On the other side, due to high rotational speed, these assemblies have to be sealed contactlessly, by means of labyrinth, centrifugal or similar types of seals. These seals operate with very small gaps between their rotor and stator. In order to obtain the lowest possible gap in the sealing which allows displacements of the shaft supported by one elastic and one stiff support, a specific design solution is developed. Testing procedure and results, together with design solutions are presented in this paper.
C3  - 10th International Scientific Conference “IRMES 2022” “Machine design in the context of Industry 4.0 – Intelligent products” 26 May 2022, Belgrade, Serbia
T1  - Sealing of the High Speed Bearing Assemblies with One Elastic Support
EP  - 165
SP  - 162
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7639
ER  - 
@conference{
author = "Stanković, Miloš and Kolarević, Nenad and Mihajlović, Dimitrije and Ognjanović, Milosav and Davidović, Nikola and Miloš, Marko",
year = "2022",
abstract = "High speed bearing assemblies are widely applied in many industries, especially in the airspace and automotive. Design of these assemblies is highly challenging due to some opposed factors affecting their proper functionality. On the one side, there is a condition of rotor-dynamics, which implies the shaft to rotate as stable as possible, retaining its original shape. In regards to this, it was observed that having one elastic and one stiff support, rather than having two stiff supports, provides better dynamic behaviour. On the other side, due to high rotational speed, these assemblies have to be sealed contactlessly, by means of labyrinth, centrifugal or similar types of seals. These seals operate with very small gaps between their rotor and stator. In order to obtain the lowest possible gap in the sealing which allows displacements of the shaft supported by one elastic and one stiff support, a specific design solution is developed. Testing procedure and results, together with design solutions are presented in this paper.",
journal = "10th International Scientific Conference “IRMES 2022” “Machine design in the context of Industry 4.0 – Intelligent products” 26 May 2022, Belgrade, Serbia",
title = "Sealing of the High Speed Bearing Assemblies with One Elastic Support",
pages = "165-162",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7639"
}
Stanković, M., Kolarević, N., Mihajlović, D., Ognjanović, M., Davidović, N.,& Miloš, M.. (2022). Sealing of the High Speed Bearing Assemblies with One Elastic Support. in 10th International Scientific Conference “IRMES 2022” “Machine design in the context of Industry 4.0 – Intelligent products” 26 May 2022, Belgrade, Serbia, 162-165.
https://hdl.handle.net/21.15107/rcub_machinery_7639
Stanković M, Kolarević N, Mihajlović D, Ognjanović M, Davidović N, Miloš M. Sealing of the High Speed Bearing Assemblies with One Elastic Support. in 10th International Scientific Conference “IRMES 2022” “Machine design in the context of Industry 4.0 – Intelligent products” 26 May 2022, Belgrade, Serbia. 2022;:162-165.
https://hdl.handle.net/21.15107/rcub_machinery_7639 .
Stanković, Miloš, Kolarević, Nenad, Mihajlović, Dimitrije, Ognjanović, Milosav, Davidović, Nikola, Miloš, Marko, "Sealing of the High Speed Bearing Assemblies with One Elastic Support" in 10th International Scientific Conference “IRMES 2022” “Machine design in the context of Industry 4.0 – Intelligent products” 26 May 2022, Belgrade, Serbia (2022):162-165,
https://hdl.handle.net/21.15107/rcub_machinery_7639 .

Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads

Kolarević, Nenad; Stanković, Miloš; Miloš, Marko; Davidović, Nikola

(Sage Publications Ltd, London, 2022)

TY  - JOUR
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Miloš, Marko
AU  - Davidović, Nikola
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3708
AB  - The operation of gas generators brings relatively high thermo-mechanical loads on the gas generator structure. The objective of this article is to determine the operating conditions, in terms of mechanical loads at extremely high temperatures in very limited and narrow space, of a multifunctional bulkhead for application on specific kinds of gas generators with back-to-back rotor concept. The paper contains numerical analysis and experimental investigation for determining the loads and behavior of the structure. Numerical analysis indicates that there is significant influence of the Tesla turbine effect on flow parameters. Also, uneven pressure distribution and significant thermal loads are identified. With experimental investigation and subsequent exploitation tests, it was concluded that the presented methodology identifies the operating conditions, truthfully simulates the bulkhead stress state and deformations and that the presented design solution satisfied all demands. Regarding results obtained by these numerical simulations, the innovative design solution for the multifunctional bulkhead was proposed.
PB  - Sage Publications Ltd, London
T2  - Advances in Mechanical Engineering
T1  - Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads
IS  - 8
VL  - 14
DO  - 10.1177/16878132221115939
ER  - 
@article{
author = "Kolarević, Nenad and Stanković, Miloš and Miloš, Marko and Davidović, Nikola",
year = "2022",
abstract = "The operation of gas generators brings relatively high thermo-mechanical loads on the gas generator structure. The objective of this article is to determine the operating conditions, in terms of mechanical loads at extremely high temperatures in very limited and narrow space, of a multifunctional bulkhead for application on specific kinds of gas generators with back-to-back rotor concept. The paper contains numerical analysis and experimental investigation for determining the loads and behavior of the structure. Numerical analysis indicates that there is significant influence of the Tesla turbine effect on flow parameters. Also, uneven pressure distribution and significant thermal loads are identified. With experimental investigation and subsequent exploitation tests, it was concluded that the presented methodology identifies the operating conditions, truthfully simulates the bulkhead stress state and deformations and that the presented design solution satisfied all demands. Regarding results obtained by these numerical simulations, the innovative design solution for the multifunctional bulkhead was proposed.",
publisher = "Sage Publications Ltd, London",
journal = "Advances in Mechanical Engineering",
title = "Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads",
number = "8",
volume = "14",
doi = "10.1177/16878132221115939"
}
Kolarević, N., Stanković, M., Miloš, M.,& Davidović, N.. (2022). Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads. in Advances in Mechanical Engineering
Sage Publications Ltd, London., 14(8).
https://doi.org/10.1177/16878132221115939
Kolarević N, Stanković M, Miloš M, Davidović N. Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads. in Advances in Mechanical Engineering. 2022;14(8).
doi:10.1177/16878132221115939 .
Kolarević, Nenad, Stanković, Miloš, Miloš, Marko, Davidović, Nikola, "Analysis and design of the gas generator multifunctional bulkhead considering the thermal and structural loads" in Advances in Mechanical Engineering, 14, no. 8 (2022),
https://doi.org/10.1177/16878132221115939 . .
1
1

Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System

Đorđević, Aleksandar; Premović-Zecević, Milena; Minić, Dusko; Manasijević, Dragan; Radicević, Branko; Kolarević, Nenad; Ristić, Vladica

(Springer, New York, 2022)

TY  - JOUR
AU  - Đorđević, Aleksandar
AU  - Premović-Zecević, Milena
AU  - Minić, Dusko
AU  - Manasijević, Dragan
AU  - Radicević, Branko
AU  - Kolarević, Nenad
AU  - Ristić, Vladica
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3701
AB  - In the current study the ternary Ga-Ge-Zn system was experimentally and analytically tested. The ternary system is chosen due to the importance of germanium-based alloys in the electronic industry and their special application as memory materials. There are no previous studies related to the Ga-Ge-Zn system up to this paper. Used experimental techniques were differential thermal analysis, scanning electron microscopy with energy dispersive spectrometry, x-ray powder diffraction, electrical conductivity and hardness tests. The experimentally obtained results were compared with the results of thermodynamic calculation of phase equilibria using the calculation of phase diagram (CALPHAD) method and literature data. Calculated phase diagrams were three vertical sections (Ga-GeZn, Ge-GaZn and Zn-GaGe), three isothermal sections (100, 200 and 300 degrees C) and liquidus projection with invariant reactions. Good agreements between calculated phase diagrams and experimental data have been obtained without introducing ternary thermodynamic parameters.
PB  - Springer, New York
T2  - Journal of Phase Equilibria and Diffusion
T1  - Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System
EP  - 192
IS  - 2
SP  - 176
VL  - 43
DO  - 10.1007/s11669-022-00952-x
ER  - 
@article{
author = "Đorđević, Aleksandar and Premović-Zecević, Milena and Minić, Dusko and Manasijević, Dragan and Radicević, Branko and Kolarević, Nenad and Ristić, Vladica",
year = "2022",
abstract = "In the current study the ternary Ga-Ge-Zn system was experimentally and analytically tested. The ternary system is chosen due to the importance of germanium-based alloys in the electronic industry and their special application as memory materials. There are no previous studies related to the Ga-Ge-Zn system up to this paper. Used experimental techniques were differential thermal analysis, scanning electron microscopy with energy dispersive spectrometry, x-ray powder diffraction, electrical conductivity and hardness tests. The experimentally obtained results were compared with the results of thermodynamic calculation of phase equilibria using the calculation of phase diagram (CALPHAD) method and literature data. Calculated phase diagrams were three vertical sections (Ga-GeZn, Ge-GaZn and Zn-GaGe), three isothermal sections (100, 200 and 300 degrees C) and liquidus projection with invariant reactions. Good agreements between calculated phase diagrams and experimental data have been obtained without introducing ternary thermodynamic parameters.",
publisher = "Springer, New York",
journal = "Journal of Phase Equilibria and Diffusion",
title = "Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System",
pages = "192-176",
number = "2",
volume = "43",
doi = "10.1007/s11669-022-00952-x"
}
Đorđević, A., Premović-Zecević, M., Minić, D., Manasijević, D., Radicević, B., Kolarević, N.,& Ristić, V.. (2022). Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System. in Journal of Phase Equilibria and Diffusion
Springer, New York., 43(2), 176-192.
https://doi.org/10.1007/s11669-022-00952-x
Đorđević A, Premović-Zecević M, Minić D, Manasijević D, Radicević B, Kolarević N, Ristić V. Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System. in Journal of Phase Equilibria and Diffusion. 2022;43(2):176-192.
doi:10.1007/s11669-022-00952-x .
Đorđević, Aleksandar, Premović-Zecević, Milena, Minić, Dusko, Manasijević, Dragan, Radicević, Branko, Kolarević, Nenad, Ristić, Vladica, "Experimental Study of the Phase Equilibria in the Ternary Ga-Ge-Zn System" in Journal of Phase Equilibria and Diffusion, 43, no. 2 (2022):176-192,
https://doi.org/10.1007/s11669-022-00952-x . .

Research of expendable turbojet tubular combustion chamber

Davidović, Nikola; Kolarević, Nenad; Stanković, Miloš; Miloš, Marko

(Sage Publications Ltd, London, 2022)

TY  - JOUR
AU  - Davidović, Nikola
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Miloš, Marko
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3688
AB  - This paper presents research related to the tubular combustion chamber of an expendable turbojet. Although annular combustors are dominant at present, tubular combustors are still attractive because they are simpler to produce and require lower amounts of air flow for testing. The objective of this research was to assess the combustor's primary zone configuration, and four configurations were tested to obtain experimental answers for use in future work. The configuration of the combustion chamber is a simple and classic design in line with its expendable purpose. The test methodology was to perform initial testing of the primary and secondary zones under atmospheric conditions using the four configurations, and then to subsequently complete the combustor using the best configuration. The complete combustor was then tested under both atmospheric conditions and working conditions. The results showed that the stability margin was wide enough to cover the combustor's entire working area. The measured efficiency and pressure drop were in very good agreement with the corresponding designed values. The design and testing methodology proposed here could be used for similar scientific and engineering research applications.
PB  - Sage Publications Ltd, London
T2  - Advances in Mechanical Engineering
T1  - Research of expendable turbojet tubular combustion chamber
IS  - 5
VL  - 14
DO  - 10.1177/16878132221095999
ER  - 
@article{
author = "Davidović, Nikola and Kolarević, Nenad and Stanković, Miloš and Miloš, Marko",
year = "2022",
abstract = "This paper presents research related to the tubular combustion chamber of an expendable turbojet. Although annular combustors are dominant at present, tubular combustors are still attractive because they are simpler to produce and require lower amounts of air flow for testing. The objective of this research was to assess the combustor's primary zone configuration, and four configurations were tested to obtain experimental answers for use in future work. The configuration of the combustion chamber is a simple and classic design in line with its expendable purpose. The test methodology was to perform initial testing of the primary and secondary zones under atmospheric conditions using the four configurations, and then to subsequently complete the combustor using the best configuration. The complete combustor was then tested under both atmospheric conditions and working conditions. The results showed that the stability margin was wide enough to cover the combustor's entire working area. The measured efficiency and pressure drop were in very good agreement with the corresponding designed values. The design and testing methodology proposed here could be used for similar scientific and engineering research applications.",
publisher = "Sage Publications Ltd, London",
journal = "Advances in Mechanical Engineering",
title = "Research of expendable turbojet tubular combustion chamber",
number = "5",
volume = "14",
doi = "10.1177/16878132221095999"
}
Davidović, N., Kolarević, N., Stanković, M.,& Miloš, M.. (2022). Research of expendable turbojet tubular combustion chamber. in Advances in Mechanical Engineering
Sage Publications Ltd, London., 14(5).
https://doi.org/10.1177/16878132221095999
Davidović N, Kolarević N, Stanković M, Miloš M. Research of expendable turbojet tubular combustion chamber. in Advances in Mechanical Engineering. 2022;14(5).
doi:10.1177/16878132221095999 .
Davidović, Nikola, Kolarević, Nenad, Stanković, Miloš, Miloš, Marko, "Research of expendable turbojet tubular combustion chamber" in Advances in Mechanical Engineering, 14, no. 5 (2022),
https://doi.org/10.1177/16878132221095999 . .
1
1

Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling

Premović, Milena; Đorđević, Aleksandar; Minić, Dusko; Manasijević, Dragan; Radicević, Branko; Kolarević, Nenad; Ristić, Vladica

(Pergamon-Elsevier Science Ltd, Oxford, 2022)

TY  - JOUR
AU  - Premović, Milena
AU  - Đorđević, Aleksandar
AU  - Minić, Dusko
AU  - Manasijević, Dragan
AU  - Radicević, Branko
AU  - Kolarević, Nenad
AU  - Ristić, Vladica
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3721
AB  - The ternary Ge-In-Zn system is chosen for the study due to the importance of germanium-based alloys in the industry of electronic devices and their special application as memory materials. This ternary system has not been explored so far. In the current work, experimental techniques such as differential thermal analysis (DTA), scanning electron microscopy (SEM) with energy dispersive spectrometry (EDS), X-ray powder diffraction (XRD) and electrical conductivity tests were used for characterization of the prepared ternary Ge-In-Zn alloys. Investigated alloys were from four isothermal sections at 25, 100, 200 and 300 degrees C and three vertical sections Ge-InZn, In-GeZn, Zn-GeIn. The obtained results were compared with the results of thermodynamic calculation of phase equilibria based on the Calphad method. The calculation was performed by using thermodynamic parameters for constitutive binary systems. Good agreements between calculated phase diagrams and experimental data have been obtained without introducing ternary thermodynamic parameters. Based on that, calculations of liquidus projection and invariant reactions were performed.
PB  - Pergamon-Elsevier Science Ltd, Oxford
T2  - Calphad-Computer Coupling of Phase Diagrams and Thermochemistry
T1  - Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling
VL  - 77
DO  - 10.1016/j.calphad.2022.102432
ER  - 
@article{
author = "Premović, Milena and Đorđević, Aleksandar and Minić, Dusko and Manasijević, Dragan and Radicević, Branko and Kolarević, Nenad and Ristić, Vladica",
year = "2022",
abstract = "The ternary Ge-In-Zn system is chosen for the study due to the importance of germanium-based alloys in the industry of electronic devices and their special application as memory materials. This ternary system has not been explored so far. In the current work, experimental techniques such as differential thermal analysis (DTA), scanning electron microscopy (SEM) with energy dispersive spectrometry (EDS), X-ray powder diffraction (XRD) and electrical conductivity tests were used for characterization of the prepared ternary Ge-In-Zn alloys. Investigated alloys were from four isothermal sections at 25, 100, 200 and 300 degrees C and three vertical sections Ge-InZn, In-GeZn, Zn-GeIn. The obtained results were compared with the results of thermodynamic calculation of phase equilibria based on the Calphad method. The calculation was performed by using thermodynamic parameters for constitutive binary systems. Good agreements between calculated phase diagrams and experimental data have been obtained without introducing ternary thermodynamic parameters. Based on that, calculations of liquidus projection and invariant reactions were performed.",
publisher = "Pergamon-Elsevier Science Ltd, Oxford",
journal = "Calphad-Computer Coupling of Phase Diagrams and Thermochemistry",
title = "Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling",
volume = "77",
doi = "10.1016/j.calphad.2022.102432"
}
Premović, M., Đorđević, A., Minić, D., Manasijević, D., Radicević, B., Kolarević, N.,& Ristić, V.. (2022). Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling. in Calphad-Computer Coupling of Phase Diagrams and Thermochemistry
Pergamon-Elsevier Science Ltd, Oxford., 77.
https://doi.org/10.1016/j.calphad.2022.102432
Premović M, Đorđević A, Minić D, Manasijević D, Radicević B, Kolarević N, Ristić V. Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling. in Calphad-Computer Coupling of Phase Diagrams and Thermochemistry. 2022;77.
doi:10.1016/j.calphad.2022.102432 .
Premović, Milena, Đorđević, Aleksandar, Minić, Dusko, Manasijević, Dragan, Radicević, Branko, Kolarević, Nenad, Ristić, Vladica, "Thermodynamic description and electrical conductivity of the Ge-In-Zn system: Experiments and modeling" in Calphad-Computer Coupling of Phase Diagrams and Thermochemistry, 77 (2022),
https://doi.org/10.1016/j.calphad.2022.102432 . .
1

Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist

Stanković, Miloš; Kolarević, Nenad; Davidović, Nikola; Miloš, Marko

(Emerald Group Publishing Ltd, Bingley, 2022)

TY  - JOUR
AU  - Stanković, Miloš
AU  - Kolarević, Nenad
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2022
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3754
AB  - Purpose The purpose of this paper is to improve the lubrication and remove as much as possible of the heat generated in the bearing assembly, embedded in the jet engine. Design/methodology/approach To determine the necessary values of the air pressure and oil amount, an experimental approach is used. For that purpose, a custom made test rig is developed. Findings Less amount of oil makes better lubrication conditions, reflected in the smaller temperature of the bearings. Concerning the air pressure, too high and too low air pressure deteriorates the lubrication parameters. An optimum value should be determined experimentally. The influence of oil amount is remarkably bigger than the influence of air pressure. Originality/value This experimental investigation provides an easy and fast way to improve the high-speed bearings lubrication parameters.
PB  - Emerald Group Publishing Ltd, Bingley
T2  - Industrial Lubrication and Tribology
T1  - Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist
EP  - 341
IS  - 3
SP  - 335
VL  - 74
DO  - 10.1108/ILT-06-2021-0222
ER  - 
@article{
author = "Stanković, Miloš and Kolarević, Nenad and Davidović, Nikola and Miloš, Marko",
year = "2022",
abstract = "Purpose The purpose of this paper is to improve the lubrication and remove as much as possible of the heat generated in the bearing assembly, embedded in the jet engine. Design/methodology/approach To determine the necessary values of the air pressure and oil amount, an experimental approach is used. For that purpose, a custom made test rig is developed. Findings Less amount of oil makes better lubrication conditions, reflected in the smaller temperature of the bearings. Concerning the air pressure, too high and too low air pressure deteriorates the lubrication parameters. An optimum value should be determined experimentally. The influence of oil amount is remarkably bigger than the influence of air pressure. Originality/value This experimental investigation provides an easy and fast way to improve the high-speed bearings lubrication parameters.",
publisher = "Emerald Group Publishing Ltd, Bingley",
journal = "Industrial Lubrication and Tribology",
title = "Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist",
pages = "341-335",
number = "3",
volume = "74",
doi = "10.1108/ILT-06-2021-0222"
}
Stanković, M., Kolarević, N., Davidović, N.,& Miloš, M.. (2022). Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist. in Industrial Lubrication and Tribology
Emerald Group Publishing Ltd, Bingley., 74(3), 335-341.
https://doi.org/10.1108/ILT-06-2021-0222
Stanković M, Kolarević N, Davidović N, Miloš M. Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist. in Industrial Lubrication and Tribology. 2022;74(3):335-341.
doi:10.1108/ILT-06-2021-0222 .
Stanković, Miloš, Kolarević, Nenad, Davidović, Nikola, Miloš, Marko, "Influence of the air pressure and oil amount to the temperature of the high-speed bearings lubricated by oil mist" in Industrial Lubrication and Tribology, 74, no. 3 (2022):335-341,
https://doi.org/10.1108/ILT-06-2021-0222 . .
1
1
1

Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist

Stanković, Miloš; Kolarević, Nenad; Davidović, Nikola; Miloš, Marko

(2021)

TY  - CONF
AU  - Stanković, Miloš
AU  - Kolarević, Nenad
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7635
AB  - High speed bearing assemblies have been always challenging in terms of the heat removal and bearing lubrication. Evolution of these lubrication systems led to the oil-mist concept, which consists of the air under high pressure, together with oil droplets. Too high pressure combined with too much of oil would cause the additional resistance to the rolling elements’ movement, while the low pressure with the small amount of oil wouldn’t be effective in terms of the heat removal and lubrication. In this paper, it is analysed the influence of the air pressure and the amount of oil onto the bearings’ temperature.
C3  - 10th International Conference on Tribology – BALKANTRIB '20
T1  - Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist
EP  - 116
SP  - 115
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7635
ER  - 
@conference{
author = "Stanković, Miloš and Kolarević, Nenad and Davidović, Nikola and Miloš, Marko",
year = "2021",
abstract = "High speed bearing assemblies have been always challenging in terms of the heat removal and bearing lubrication. Evolution of these lubrication systems led to the oil-mist concept, which consists of the air under high pressure, together with oil droplets. Too high pressure combined with too much of oil would cause the additional resistance to the rolling elements’ movement, while the low pressure with the small amount of oil wouldn’t be effective in terms of the heat removal and lubrication. In this paper, it is analysed the influence of the air pressure and the amount of oil onto the bearings’ temperature.",
journal = "10th International Conference on Tribology – BALKANTRIB '20",
title = "Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist",
pages = "116-115",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7635"
}
Stanković, M., Kolarević, N., Davidović, N.,& Miloš, M.. (2021). Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist. in 10th International Conference on Tribology – BALKANTRIB '20, 115-116.
https://hdl.handle.net/21.15107/rcub_machinery_7635
Stanković M, Kolarević N, Davidović N, Miloš M. Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist. in 10th International Conference on Tribology – BALKANTRIB '20. 2021;:115-116.
https://hdl.handle.net/21.15107/rcub_machinery_7635 .
Stanković, Miloš, Kolarević, Nenad, Davidović, Nikola, Miloš, Marko, "Experimental Investigation of the High-Speed Roller Bearing Assembly Lubricated by Oil Mist" in 10th International Conference on Tribology – BALKANTRIB '20 (2021):115-116,
https://hdl.handle.net/21.15107/rcub_machinery_7635 .

Experimental Validation of Rotordynamics for High Speed Machines

Kolarević, Nenad; Stanković, Miloš; Davidović, Nikola; Miloš, Marko

(2021)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7636
C3  - 37th Danubia-Adria Symposium on Advances in Experimental Mechanics, 21. − 24. September 2021, Linz, Austria
T1  - Experimental Validation of Rotordynamics for High Speed Machines
EP  - 95
SP  - 94
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7636
ER  - 
@conference{
author = "Kolarević, Nenad and Stanković, Miloš and Davidović, Nikola and Miloš, Marko",
year = "2021",
journal = "37th Danubia-Adria Symposium on Advances in Experimental Mechanics, 21. − 24. September 2021, Linz, Austria",
title = "Experimental Validation of Rotordynamics for High Speed Machines",
pages = "95-94",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7636"
}
Kolarević, N., Stanković, M., Davidović, N.,& Miloš, M.. (2021). Experimental Validation of Rotordynamics for High Speed Machines. in 37th Danubia-Adria Symposium on Advances in Experimental Mechanics, 21. − 24. September 2021, Linz, Austria, 94-95.
https://hdl.handle.net/21.15107/rcub_machinery_7636
Kolarević N, Stanković M, Davidović N, Miloš M. Experimental Validation of Rotordynamics for High Speed Machines. in 37th Danubia-Adria Symposium on Advances in Experimental Mechanics, 21. − 24. September 2021, Linz, Austria. 2021;:94-95.
https://hdl.handle.net/21.15107/rcub_machinery_7636 .
Kolarević, Nenad, Stanković, Miloš, Davidović, Nikola, Miloš, Marko, "Experimental Validation of Rotordynamics for High Speed Machines" in 37th Danubia-Adria Symposium on Advances in Experimental Mechanics, 21. − 24. September 2021, Linz, Austria (2021):94-95,
https://hdl.handle.net/21.15107/rcub_machinery_7636 .

Study of innovative subsonic ramjet

Davidović, Nikola; Miloš, Predrag; Kolarević, Nenad; Ivanov, Toni; Jojić, Branislav

(Springer, 2021)

TY  - CHAP
AU  - Davidović, Nikola
AU  - Miloš, Predrag
AU  - Kolarević, Nenad
AU  - Ivanov, Toni
AU  - Jojić, Branislav
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3675
AB  - Subsonic ramjets, due to its simplicity, nowadays could be very attractive for expendable unmanned applications. However, due to very low efficiency at low Mach numbers, practically there isn’t any important application at subsonic speed. In 50’s subsonic ramjet was used for tip jet applications. Later in 70’s there was a study of Fan Augmented Ramjet (FARJ) where a fan was in-tended to be powered by a piston engine, both in subsonic and supersonic regimes. Almost at the same time it was analyzed ejector augmented subsonic ramjet. Both of these studies did not find real application of such engines. Finally, there was an attempt for the use of an Electric Ducted Fan, used in RC models, with a combustor but exit fan pressure was almost at atmospheric pressure which results in very low efficiency. This paper presents a study of propulsion system which consists of a pitot intake, electrically powered compressor/fan, combustor and nozzle (Electrically Fan Augmented Ram Jet, EFARJ). The electric motor connection to the compressor/fan is direct, without gearbox, which implies usage of a high-speed brushless motor. Such propulsion system is compared to pure ramjet and finally it is compared to performances of small expendable turbojet. Comparison is made regarding costs, weight and thrust/consumption. The study shows that the proposed propulsion system could be competitive for expendable, low speed and short duration applications.
PB  - Springer
T2  - Lecture Notes in Networks and Systems
T1  - Study of innovative subsonic ramjet
EP  - 431
SP  - 413
VL  - 153
DO  - 10.1007/978-3-030-58362-0_24
ER  - 
@inbook{
author = "Davidović, Nikola and Miloš, Predrag and Kolarević, Nenad and Ivanov, Toni and Jojić, Branislav",
year = "2021",
abstract = "Subsonic ramjets, due to its simplicity, nowadays could be very attractive for expendable unmanned applications. However, due to very low efficiency at low Mach numbers, practically there isn’t any important application at subsonic speed. In 50’s subsonic ramjet was used for tip jet applications. Later in 70’s there was a study of Fan Augmented Ramjet (FARJ) where a fan was in-tended to be powered by a piston engine, both in subsonic and supersonic regimes. Almost at the same time it was analyzed ejector augmented subsonic ramjet. Both of these studies did not find real application of such engines. Finally, there was an attempt for the use of an Electric Ducted Fan, used in RC models, with a combustor but exit fan pressure was almost at atmospheric pressure which results in very low efficiency. This paper presents a study of propulsion system which consists of a pitot intake, electrically powered compressor/fan, combustor and nozzle (Electrically Fan Augmented Ram Jet, EFARJ). The electric motor connection to the compressor/fan is direct, without gearbox, which implies usage of a high-speed brushless motor. Such propulsion system is compared to pure ramjet and finally it is compared to performances of small expendable turbojet. Comparison is made regarding costs, weight and thrust/consumption. The study shows that the proposed propulsion system could be competitive for expendable, low speed and short duration applications.",
publisher = "Springer",
journal = "Lecture Notes in Networks and Systems",
booktitle = "Study of innovative subsonic ramjet",
pages = "431-413",
volume = "153",
doi = "10.1007/978-3-030-58362-0_24"
}
Davidović, N., Miloš, P., Kolarević, N., Ivanov, T.,& Jojić, B.. (2021). Study of innovative subsonic ramjet. in Lecture Notes in Networks and Systems
Springer., 153, 413-431.
https://doi.org/10.1007/978-3-030-58362-0_24
Davidović N, Miloš P, Kolarević N, Ivanov T, Jojić B. Study of innovative subsonic ramjet. in Lecture Notes in Networks and Systems. 2021;153:413-431.
doi:10.1007/978-3-030-58362-0_24 .
Davidović, Nikola, Miloš, Predrag, Kolarević, Nenad, Ivanov, Toni, Jojić, Branislav, "Study of innovative subsonic ramjet" in Lecture Notes in Networks and Systems, 153 (2021):413-431,
https://doi.org/10.1007/978-3-030-58362-0_24 . .
1

Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters

Kolarević, Nenad; Stanković, Miloš; Davidović, Nikola; Miloš, Marko

(2020)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Davidović, Nikola
AU  - Miloš, Marko
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7638
AB  - If one compares the tip-jet helicopters to the conventional ones, one of the most important disadvantages are the much heavier blades, due to the massive inner channel for operating fluid transport through its structure. This increased blade mass causes a significantly larger centrifugal force that loads the construction of the rotor head, especially the feathering and teetering hinge. The case study of this paper is feathering hinge assembly of teetering rotor head for ultra-light tip-jet unmanned helicopter. The new design solution and structural optimization for such engineering problem is presented in this paper. The described construction solution is developed for a new project of unmanned helicopter Hussar based on the experience and knowledge achieved on the previous helicopters ATRO-X and Hornet.
C3  - 9th International Scientific Conference on Defensive Technologies - OTEH
T1  - Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters
EP  - 128
SP  - 123
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7638
ER  - 
@conference{
author = "Kolarević, Nenad and Stanković, Miloš and Davidović, Nikola and Miloš, Marko",
year = "2020",
abstract = "If one compares the tip-jet helicopters to the conventional ones, one of the most important disadvantages are the much heavier blades, due to the massive inner channel for operating fluid transport through its structure. This increased blade mass causes a significantly larger centrifugal force that loads the construction of the rotor head, especially the feathering and teetering hinge. The case study of this paper is feathering hinge assembly of teetering rotor head for ultra-light tip-jet unmanned helicopter. The new design solution and structural optimization for such engineering problem is presented in this paper. The described construction solution is developed for a new project of unmanned helicopter Hussar based on the experience and knowledge achieved on the previous helicopters ATRO-X and Hornet.",
journal = "9th International Scientific Conference on Defensive Technologies - OTEH",
title = "Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters",
pages = "128-123",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7638"
}
Kolarević, N., Stanković, M., Davidović, N.,& Miloš, M.. (2020). Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters. in 9th International Scientific Conference on Defensive Technologies - OTEH, 123-128.
https://hdl.handle.net/21.15107/rcub_machinery_7638
Kolarević N, Stanković M, Davidović N, Miloš M. Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters. in 9th International Scientific Conference on Defensive Technologies - OTEH. 2020;:123-128.
https://hdl.handle.net/21.15107/rcub_machinery_7638 .
Kolarević, Nenad, Stanković, Miloš, Davidović, Nikola, Miloš, Marko, "Design Solution and Structural Optimisation of Feathering Hinge Assembly of Teetering Rotor Head for Tip-Jet Helicopters" in 9th International Scientific Conference on Defensive Technologies - OTEH (2020):123-128,
https://hdl.handle.net/21.15107/rcub_machinery_7638 .

Mechanical and electrical properties of the Bi-Ge-Sn alloys

Đorđević, Aleksandar; Premović, Milena; Minić, Duško; Tomović, Milica; Radičević, Branko; Kolarević, Nenad

(The Netherlands Press, 2020)

TY  - JOUR
AU  - Đorđević, Aleksandar
AU  - Premović, Milena
AU  - Minić, Duško
AU  - Tomović, Milica
AU  - Radičević, Branko
AU  - Kolarević, Nenad
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/6329
AB  - Mechanical   and   electrical properties   of   the   ternary   Bi-Ge-Sn   alloys   were investigated in this study. Calculation of isothermal section at 200, 300, and 25 ºC was carried  out  by  using  optimized  thermodynamic  parameters  for  the  constitutive  binary systems.  Microstructures  of  alloys  were  observed  by  using  optical  microscopy  and scanning electron  microscopy (SEM). Phases in  microstructures have  been detected by X-ray  diffraction  (XRD)  analysis  and  compositions  of  the  phase  by  energy  dispersive spectrometry (EDS). EDS results were compared with the predicted isothermal section at 200  and  300  ºC,  and  good  agreement  has  been  reached  between  them.  The  Brinell hardness and electrical conductivity of selected alloys were measured.  Through ANOVA analysis  and  application  of  the  obtained  results,  an  appropriate  mathematical  model  is proposed for every composition of alloys. By using the appropriated mathematical model for  Brinell  hardness  and  electrical  conductivity,  isolines  for  those  properties  were presented.
PB  - The Netherlands Press
T2  - Metallurgical and Materials Engineering
T1  - Mechanical and electrical properties of the Bi-Ge-Sn alloys
EP  - 415
IS  - 26
SP  - 395
VL  - 26
DO  - 10.30544/562
ER  - 
@article{
author = "Đorđević, Aleksandar and Premović, Milena and Minić, Duško and Tomović, Milica and Radičević, Branko and Kolarević, Nenad",
year = "2020",
abstract = "Mechanical   and   electrical properties   of   the   ternary   Bi-Ge-Sn   alloys   were investigated in this study. Calculation of isothermal section at 200, 300, and 25 ºC was carried  out  by  using  optimized  thermodynamic  parameters  for  the  constitutive  binary systems.  Microstructures  of  alloys  were  observed  by  using  optical  microscopy  and scanning electron  microscopy (SEM). Phases in  microstructures have  been detected by X-ray  diffraction  (XRD)  analysis  and  compositions  of  the  phase  by  energy  dispersive spectrometry (EDS). EDS results were compared with the predicted isothermal section at 200  and  300  ºC,  and  good  agreement  has  been  reached  between  them.  The  Brinell hardness and electrical conductivity of selected alloys were measured.  Through ANOVA analysis  and  application  of  the  obtained  results,  an  appropriate  mathematical  model  is proposed for every composition of alloys. By using the appropriated mathematical model for  Brinell  hardness  and  electrical  conductivity,  isolines  for  those  properties  were presented.",
publisher = "The Netherlands Press",
journal = "Metallurgical and Materials Engineering",
title = "Mechanical and electrical properties of the Bi-Ge-Sn alloys",
pages = "415-395",
number = "26",
volume = "26",
doi = "10.30544/562"
}
Đorđević, A., Premović, M., Minić, D., Tomović, M., Radičević, B.,& Kolarević, N.. (2020). Mechanical and electrical properties of the Bi-Ge-Sn alloys. in Metallurgical and Materials Engineering
The Netherlands Press., 26(26), 395-415.
https://doi.org/10.30544/562
Đorđević A, Premović M, Minić D, Tomović M, Radičević B, Kolarević N. Mechanical and electrical properties of the Bi-Ge-Sn alloys. in Metallurgical and Materials Engineering. 2020;26(26):395-415.
doi:10.30544/562 .
Đorđević, Aleksandar, Premović, Milena, Minić, Duško, Tomović, Milica, Radičević, Branko, Kolarević, Nenad, "Mechanical and electrical properties of the Bi-Ge-Sn alloys" in Metallurgical and Materials Engineering, 26, no. 26 (2020):395-415,
https://doi.org/10.30544/562 . .

Experimental verification of performance of tip-jet helicopter propulsion system

Kolarević, Nenad; Crnojević, Stevan; Stanković, Miloš; Latković, Nenad; Miloš, Marko

(Elsevier, Amsterdam, 2020)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Crnojević, Stevan
AU  - Stanković, Miloš
AU  - Latković, Nenad
AU  - Miloš, Marko
PY  - 2020
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3315
AB  - This paper presents the methodology for estimation of power delivery and efficiency of the tip-jet helicopter propulsion system. The main advantage of the tip-jet helicopter is the absence of heavy transmission and tail rotor, but if compared to conventional helicopters, it has significantly lower efficiency. The crucial parameter that impacts the performances of the tip-jet helicopter is a propulsion force at the end of the blade. The analytical and numerical calculations with results for prediction of this propulsion force are presented in this paper. The case study is the ATRO-X tip-jet helicopter. Its propulsion system is driven by the gas-generator Phoenix-100, as a power source, which generates propulsion force by ejecting the hot combustion products through the nozzles at the blades tips.
PB  - Elsevier, Amsterdam
C3  - Materials Today-Proceedings
T1  - Experimental verification of performance of tip-jet helicopter propulsion system
EP  - 117
SP  - 112
VL  - 32
DO  - 10.1016/j.matpr.2020.03.080
ER  - 
@conference{
author = "Kolarević, Nenad and Crnojević, Stevan and Stanković, Miloš and Latković, Nenad and Miloš, Marko",
year = "2020",
abstract = "This paper presents the methodology for estimation of power delivery and efficiency of the tip-jet helicopter propulsion system. The main advantage of the tip-jet helicopter is the absence of heavy transmission and tail rotor, but if compared to conventional helicopters, it has significantly lower efficiency. The crucial parameter that impacts the performances of the tip-jet helicopter is a propulsion force at the end of the blade. The analytical and numerical calculations with results for prediction of this propulsion force are presented in this paper. The case study is the ATRO-X tip-jet helicopter. Its propulsion system is driven by the gas-generator Phoenix-100, as a power source, which generates propulsion force by ejecting the hot combustion products through the nozzles at the blades tips.",
publisher = "Elsevier, Amsterdam",
journal = "Materials Today-Proceedings",
title = "Experimental verification of performance of tip-jet helicopter propulsion system",
pages = "117-112",
volume = "32",
doi = "10.1016/j.matpr.2020.03.080"
}
Kolarević, N., Crnojević, S., Stanković, M., Latković, N.,& Miloš, M.. (2020). Experimental verification of performance of tip-jet helicopter propulsion system. in Materials Today-Proceedings
Elsevier, Amsterdam., 32, 112-117.
https://doi.org/10.1016/j.matpr.2020.03.080
Kolarević N, Crnojević S, Stanković M, Latković N, Miloš M. Experimental verification of performance of tip-jet helicopter propulsion system. in Materials Today-Proceedings. 2020;32:112-117.
doi:10.1016/j.matpr.2020.03.080 .
Kolarević, Nenad, Crnojević, Stevan, Stanković, Miloš, Latković, Nenad, Miloš, Marko, "Experimental verification of performance of tip-jet helicopter propulsion system" in Materials Today-Proceedings, 32 (2020):112-117,
https://doi.org/10.1016/j.matpr.2020.03.080 . .
3
2

Wear simulation of the polymer based composite sliding bearings by means of ansys

Stanković, Miloš; Marinković, Aleksandar; Kolarević, Nenad

(Faculty of Engineering, University of Kragujevac, 2019)

TY  - JOUR
AU  - Stanković, Miloš
AU  - Marinković, Aleksandar
AU  - Kolarević, Nenad
PY  - 2019
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3204
AB  - Polymer based composite sliding bearings are increasingly applied in many industries, due to their economic (usually low cost of production) and technical (good tribological properties) benefits. In order to predict their life cycle, it is necessary to perform numerous experiments and evaluate their wear rate. This is generally quite expensive and time consuming. By applying only one series of the experiments and determining Archard’s wear coefficient, and embedding it into the code of the Ansys software, it is possible to simulate the wear, and thus save the time and the financial resources. This paper explains the procedure of the wear simulation in case of known Archard’s coefficient, for sliding bearings made of PTFE polyamide composite material in contact with shaft of steel. The output of the simulation is the contact pressure in relation of time and the amount of worn volume for 3 revolutions of the shaft.
PB  - Faculty of Engineering, University of Kragujevac
T2  - Proceedings on Engineering Sciences
T1  - Wear simulation of the polymer based composite sliding bearings by means of ansys
EP  - 69
IS  - 1
SP  - 66
VL  - 1
DO  - 10.24874/PES01.01.008
ER  - 
@article{
author = "Stanković, Miloš and Marinković, Aleksandar and Kolarević, Nenad",
year = "2019",
abstract = "Polymer based composite sliding bearings are increasingly applied in many industries, due to their economic (usually low cost of production) and technical (good tribological properties) benefits. In order to predict their life cycle, it is necessary to perform numerous experiments and evaluate their wear rate. This is generally quite expensive and time consuming. By applying only one series of the experiments and determining Archard’s wear coefficient, and embedding it into the code of the Ansys software, it is possible to simulate the wear, and thus save the time and the financial resources. This paper explains the procedure of the wear simulation in case of known Archard’s coefficient, for sliding bearings made of PTFE polyamide composite material in contact with shaft of steel. The output of the simulation is the contact pressure in relation of time and the amount of worn volume for 3 revolutions of the shaft.",
publisher = "Faculty of Engineering, University of Kragujevac",
journal = "Proceedings on Engineering Sciences",
title = "Wear simulation of the polymer based composite sliding bearings by means of ansys",
pages = "69-66",
number = "1",
volume = "1",
doi = "10.24874/PES01.01.008"
}
Stanković, M., Marinković, A.,& Kolarević, N.. (2019). Wear simulation of the polymer based composite sliding bearings by means of ansys. in Proceedings on Engineering Sciences
Faculty of Engineering, University of Kragujevac., 1(1), 66-69.
https://doi.org/10.24874/PES01.01.008
Stanković M, Marinković A, Kolarević N. Wear simulation of the polymer based composite sliding bearings by means of ansys. in Proceedings on Engineering Sciences. 2019;1(1):66-69.
doi:10.24874/PES01.01.008 .
Stanković, Miloš, Marinković, Aleksandar, Kolarević, Nenad, "Wear simulation of the polymer based composite sliding bearings by means of ansys" in Proceedings on Engineering Sciences, 1, no. 1 (2019):66-69,
https://doi.org/10.24874/PES01.01.008 . .
1

Indirect approach of measuring the axial force on turbo-jet engine rotor

Kolarević, Nenad; Crnojević, Stevan; Stanković, Miloš; Miloš, Marko

(Elsevier Ltd, 2019)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Crnojević, Stevan
AU  - Stanković, Miloš
AU  - Miloš, Marko
PY  - 2019
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3196
AB  - This paper describes a new approach for measuring the axial force on a turbo-jet engine rotor from the Phoenix family. The axial force occurs due to pressure distribution from the operating fluid along the surfaces of the rotor structure. The case study is the Phoenix 100 turbo-jet engine which is specific because it has a high axial force that loads a relatively small, high speed bearings set. In order to define the maintenance period of the bearing system, it was crucial to measure this force. Since the conventional and commercial sensors were not applicable to this construction, a specific solution was created and implemented in the acquisition system and experimentally verified during the engine run on its test stand.
PB  - Elsevier Ltd
C3  - Materials Today: Proceedings
T1  - Indirect approach of measuring the axial force on turbo-jet engine rotor
EP  - 339
SP  - 335
VL  - 12
DO  - 10.1016/j.matpr.2019.03.132
ER  - 
@conference{
author = "Kolarević, Nenad and Crnojević, Stevan and Stanković, Miloš and Miloš, Marko",
year = "2019",
abstract = "This paper describes a new approach for measuring the axial force on a turbo-jet engine rotor from the Phoenix family. The axial force occurs due to pressure distribution from the operating fluid along the surfaces of the rotor structure. The case study is the Phoenix 100 turbo-jet engine which is specific because it has a high axial force that loads a relatively small, high speed bearings set. In order to define the maintenance period of the bearing system, it was crucial to measure this force. Since the conventional and commercial sensors were not applicable to this construction, a specific solution was created and implemented in the acquisition system and experimentally verified during the engine run on its test stand.",
publisher = "Elsevier Ltd",
journal = "Materials Today: Proceedings",
title = "Indirect approach of measuring the axial force on turbo-jet engine rotor",
pages = "339-335",
volume = "12",
doi = "10.1016/j.matpr.2019.03.132"
}
Kolarević, N., Crnojević, S., Stanković, M.,& Miloš, M.. (2019). Indirect approach of measuring the axial force on turbo-jet engine rotor. in Materials Today: Proceedings
Elsevier Ltd., 12, 335-339.
https://doi.org/10.1016/j.matpr.2019.03.132
Kolarević N, Crnojević S, Stanković M, Miloš M. Indirect approach of measuring the axial force on turbo-jet engine rotor. in Materials Today: Proceedings. 2019;12:335-339.
doi:10.1016/j.matpr.2019.03.132 .
Kolarević, Nenad, Crnojević, Stevan, Stanković, Miloš, Miloš, Marko, "Indirect approach of measuring the axial force on turbo-jet engine rotor" in Materials Today: Proceedings, 12 (2019):335-339,
https://doi.org/10.1016/j.matpr.2019.03.132 . .

Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system

Crnojević, Stevan; Latković, N.; Kolarević, Nenad; Miloš, Marko

(University of West Bohemia, 2019)

TY  - CONF
AU  - Crnojević, Stevan
AU  - Latković, N.
AU  - Kolarević, Nenad
AU  - Miloš, Marko
PY  - 2019
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3193
PB  - University of West Bohemia
C3  - 36th Danubia Adria Symposium on Advances in Experimental Mechanics, DAS 2019
T1  - Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system
EP  - 136
SP  - 135
UR  - https://hdl.handle.net/21.15107/rcub_machinery_3193
ER  - 
@conference{
author = "Crnojević, Stevan and Latković, N. and Kolarević, Nenad and Miloš, Marko",
year = "2019",
publisher = "University of West Bohemia",
journal = "36th Danubia Adria Symposium on Advances in Experimental Mechanics, DAS 2019",
title = "Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system",
pages = "136-135",
url = "https://hdl.handle.net/21.15107/rcub_machinery_3193"
}
Crnojević, S., Latković, N., Kolarević, N.,& Miloš, M.. (2019). Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system. in 36th Danubia Adria Symposium on Advances in Experimental Mechanics, DAS 2019
University of West Bohemia., 135-136.
https://hdl.handle.net/21.15107/rcub_machinery_3193
Crnojević S, Latković N, Kolarević N, Miloš M. Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system. in 36th Danubia Adria Symposium on Advances in Experimental Mechanics, DAS 2019. 2019;:135-136.
https://hdl.handle.net/21.15107/rcub_machinery_3193 .
Crnojević, Stevan, Latković, N., Kolarević, Nenad, Miloš, Marko, "Experimental verification of numerical simulation of the flow inside the TIP-JET helicopter propulsion system" in 36th Danubia Adria Symposium on Advances in Experimental Mechanics, DAS 2019 (2019):135-136,
https://hdl.handle.net/21.15107/rcub_machinery_3193 .

Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings

Stanković, Miloš; Marinković, Aleksandar; Kolarević, Nenad

(Univerzitet u Novom Sadu - Fakultet tehničkih nauka, Novi Sad, 2018)

TY  - JOUR
AU  - Stanković, Miloš
AU  - Marinković, Aleksandar
AU  - Kolarević, Nenad
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2762
AB  - Prediction and calculation of wear of the mechanical components in contact is one of the most important tasks in modern engineering. Due to time consumptive experiments and quite expensive test rig, it became even more challenging to evaluate wear by means of the computer simulation instead of the real experiments. With rapid improvement of the computer resources, this task became more realistic, and the results are more concurrent to those obtained by experiments. Since the most of the solvers evaluate wear by means of the Archard's equation, to perform the simulation it is mandatory to determine Archard's coefficient K. This paper provides necessary steps, experimental investigations and measurements in order to calculate Archard's coefficient K, as an input value for the simulation of wear of the polymer-based composite sleeve bearings.
PB  - Univerzitet u Novom Sadu - Fakultet tehničkih nauka, Novi Sad
T2  - Machine Design
T1  - Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings
EP  - 102
IS  - 3
SP  - 99
VL  - 10
DO  - 10.24867/MD.10.2018.3.99-102
ER  - 
@article{
author = "Stanković, Miloš and Marinković, Aleksandar and Kolarević, Nenad",
year = "2018",
abstract = "Prediction and calculation of wear of the mechanical components in contact is one of the most important tasks in modern engineering. Due to time consumptive experiments and quite expensive test rig, it became even more challenging to evaluate wear by means of the computer simulation instead of the real experiments. With rapid improvement of the computer resources, this task became more realistic, and the results are more concurrent to those obtained by experiments. Since the most of the solvers evaluate wear by means of the Archard's equation, to perform the simulation it is mandatory to determine Archard's coefficient K. This paper provides necessary steps, experimental investigations and measurements in order to calculate Archard's coefficient K, as an input value for the simulation of wear of the polymer-based composite sleeve bearings.",
publisher = "Univerzitet u Novom Sadu - Fakultet tehničkih nauka, Novi Sad",
journal = "Machine Design",
title = "Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings",
pages = "102-99",
number = "3",
volume = "10",
doi = "10.24867/MD.10.2018.3.99-102"
}
Stanković, M., Marinković, A.,& Kolarević, N.. (2018). Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings. in Machine Design
Univerzitet u Novom Sadu - Fakultet tehničkih nauka, Novi Sad., 10(3), 99-102.
https://doi.org/10.24867/MD.10.2018.3.99-102
Stanković M, Marinković A, Kolarević N. Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings. in Machine Design. 2018;10(3):99-102.
doi:10.24867/MD.10.2018.3.99-102 .
Stanković, Miloš, Marinković, Aleksandar, Kolarević, Nenad, "Calculation of the Archard's wear coefficient of the polymer-based composite sliding bearings" in Machine Design, 10, no. 3 (2018):99-102,
https://doi.org/10.24867/MD.10.2018.3.99-102 . .

Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada

Kolarević, Nenad

(Univerzitet u Beogradu, Mašinski fakultet, 2018)

TY  - THES
AU  - Kolarević, Nenad
PY  - 2018
UR  - http://eteze.bg.ac.rs/application/showtheses?thesesId=7031
UR  - https://nardus.mpn.gov.rs/handle/123456789/11622
UR  - https://fedorabg.bg.ac.rs/fedora/get/o:20640/bdef:Content/download
UR  - http://vbs.rs/scripts/cobiss?command=DISPLAY&base=70036&RID=514975395
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/56
AB  - Osnovna ideja na kojoj se zasnivaju bazni ciljevi disertacije je identifikacija ekstremno teških uslova eksploatacije mašinskih struktura i njihovih opterećenja koji predstavljaju kompleksnu interakciju izuzetno visokih toplotnih i nehomogenih uticaja, intenzivnih uticaja strujanja fluida, uticaja visokih brzina rotacije, sopstvenih i prinudnih vibracija i dr. Ovi su uticaji prisutni kod gasogeneratora turbomlaznih i turbovratilnih motora za koji je bilo potrebno razviti inovativno konstrukcijsko rešenje multifunkcionalne pregrade između rotora kompresora i turbine. Za realizaciju postavljenog cilja razvijena je odgovarajuća metodologija inženjerskog dizajna zasnovana na iterativnom razvoju, ispitivanju i analizi stanja i razaranja delova pregrade, pod nazivom Failure-based Design – FBD. Razvijen je skup od pet konstrukcijskih rešenja ove pregrade. Četvrto rešenje je postalo prihvatljivo za eksploataciju u ovim uslovima, a peto rešenje je ostvarilo sve funkcije i zadovoljilo sve zahteve. Za ovu svrhu sprovedena su mnoga eksperimentalna ispitivanja, brojne numeričke analize strujanja fluida (CFD), analiza toplotnog stanja (raspodele temperature), proračuna napona i deformacija delova pregrade, razvoj konstrukcijskih rešenja i dr. Radi realizacije osnovnog cilja, rad je obuhvatio širok spektar eksperimentalnih sadržaja, značajan broj numeričkih analiza i proračuna, analiza brojnih specifičnih havarijskih oštećenja i predloženih konstrukcijskih rešenja da bi se ova razaranja izbegla.
AB  - The general idea on which the basic goals of the dissertation are founded on is the identification of extremely hard conditions of mechanical structures and their loads which represent a complex interaction of several influences, i.e. extremely high heat, nonhomogeneous influences, intensive influences of fluid flow, high rotation speeds, its natural and forced vibrations etc. These influences are present at the gas generator of turbojet and turboshaft engines for which there was a need to develop an innovative construction solution for the multifunctional bulkhead between the compressor rotor and the turbine. In order to accomplish the set goal, an appropriate methodology of engineering design was developed which is based on iterative development, testing and analysis of the state and damage of the parts of the bulkhead, which is called Failure-based Design – FBD. A set of five construction solutions for the bulkhead was developed. The fourth solution became acceptable for exploitation in these conditions, while the fifth solution accomplished all functions and met all the requirements. In order to achieve this, numerous experimental testings were performed, along with many numerical analyses of the fluid flow (CFD), heat state (temperature distribution), stress and deformations calculations of the bulkhead parts, the development of construction solutions etc. In order to achieve basic goal, the paper encompassed a wide range of experiments, a significant number of numerical analyses and calculations, analyses of many specific damages and suggested construction solutions so as to avoid these damages.
PB  - Univerzitet u Beogradu, Mašinski fakultet
T1  - Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada
T1  - The state and behavior of dynamicaly loaded structures in extreme operating conditions
UR  - https://hdl.handle.net/21.15107/rcub_nardus_11622
ER  - 
@phdthesis{
author = "Kolarević, Nenad",
year = "2018",
abstract = "Osnovna ideja na kojoj se zasnivaju bazni ciljevi disertacije je identifikacija ekstremno teških uslova eksploatacije mašinskih struktura i njihovih opterećenja koji predstavljaju kompleksnu interakciju izuzetno visokih toplotnih i nehomogenih uticaja, intenzivnih uticaja strujanja fluida, uticaja visokih brzina rotacije, sopstvenih i prinudnih vibracija i dr. Ovi su uticaji prisutni kod gasogeneratora turbomlaznih i turbovratilnih motora za koji je bilo potrebno razviti inovativno konstrukcijsko rešenje multifunkcionalne pregrade između rotora kompresora i turbine. Za realizaciju postavljenog cilja razvijena je odgovarajuća metodologija inženjerskog dizajna zasnovana na iterativnom razvoju, ispitivanju i analizi stanja i razaranja delova pregrade, pod nazivom Failure-based Design – FBD. Razvijen je skup od pet konstrukcijskih rešenja ove pregrade. Četvrto rešenje je postalo prihvatljivo za eksploataciju u ovim uslovima, a peto rešenje je ostvarilo sve funkcije i zadovoljilo sve zahteve. Za ovu svrhu sprovedena su mnoga eksperimentalna ispitivanja, brojne numeričke analize strujanja fluida (CFD), analiza toplotnog stanja (raspodele temperature), proračuna napona i deformacija delova pregrade, razvoj konstrukcijskih rešenja i dr. Radi realizacije osnovnog cilja, rad je obuhvatio širok spektar eksperimentalnih sadržaja, značajan broj numeričkih analiza i proračuna, analiza brojnih specifičnih havarijskih oštećenja i predloženih konstrukcijskih rešenja da bi se ova razaranja izbegla., The general idea on which the basic goals of the dissertation are founded on is the identification of extremely hard conditions of mechanical structures and their loads which represent a complex interaction of several influences, i.e. extremely high heat, nonhomogeneous influences, intensive influences of fluid flow, high rotation speeds, its natural and forced vibrations etc. These influences are present at the gas generator of turbojet and turboshaft engines for which there was a need to develop an innovative construction solution for the multifunctional bulkhead between the compressor rotor and the turbine. In order to accomplish the set goal, an appropriate methodology of engineering design was developed which is based on iterative development, testing and analysis of the state and damage of the parts of the bulkhead, which is called Failure-based Design – FBD. A set of five construction solutions for the bulkhead was developed. The fourth solution became acceptable for exploitation in these conditions, while the fifth solution accomplished all functions and met all the requirements. In order to achieve this, numerous experimental testings were performed, along with many numerical analyses of the fluid flow (CFD), heat state (temperature distribution), stress and deformations calculations of the bulkhead parts, the development of construction solutions etc. In order to achieve basic goal, the paper encompassed a wide range of experiments, a significant number of numerical analyses and calculations, analyses of many specific damages and suggested construction solutions so as to avoid these damages.",
publisher = "Univerzitet u Beogradu, Mašinski fakultet",
title = "Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada, The state and behavior of dynamicaly loaded structures in extreme operating conditions",
url = "https://hdl.handle.net/21.15107/rcub_nardus_11622"
}
Kolarević, N.. (2018). Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada. 
Univerzitet u Beogradu, Mašinski fakultet..
https://hdl.handle.net/21.15107/rcub_nardus_11622
Kolarević N. Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada. 2018;.
https://hdl.handle.net/21.15107/rcub_nardus_11622 .
Kolarević, Nenad, "Stanje i ponašanje dinamički napregnutih struktura u ekstremnim uslovima rada" (2018),
https://hdl.handle.net/21.15107/rcub_nardus_11622 .

Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings

Stanković, Miloš; Marinković, Aleksandar; Kolarević, Nenad

(2018)

TY  - CONF
AU  - Stanković, Miloš
AU  - Marinković, Aleksandar
AU  - Kolarević, Nenad
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/7592
C3  - KOD 2018 – The 10th International Conference on Machine And Industrial Design In Mechanical Engineering
T1  - Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings
EP  - 137
SP  - 136
UR  - https://hdl.handle.net/21.15107/rcub_machinery_7592
ER  - 
@conference{
author = "Stanković, Miloš and Marinković, Aleksandar and Kolarević, Nenad",
year = "2018",
journal = "KOD 2018 – The 10th International Conference on Machine And Industrial Design In Mechanical Engineering",
title = "Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings",
pages = "137-136",
url = "https://hdl.handle.net/21.15107/rcub_machinery_7592"
}
Stanković, M., Marinković, A.,& Kolarević, N.. (2018). Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings. in KOD 2018 – The 10th International Conference on Machine And Industrial Design In Mechanical Engineering, 136-137.
https://hdl.handle.net/21.15107/rcub_machinery_7592
Stanković M, Marinković A, Kolarević N. Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings. in KOD 2018 – The 10th International Conference on Machine And Industrial Design In Mechanical Engineering. 2018;:136-137.
https://hdl.handle.net/21.15107/rcub_machinery_7592 .
Stanković, Miloš, Marinković, Aleksandar, Kolarević, Nenad, "Calculation of the Archard’s wear coefficient of the polymer-based composite sliding bearings" in KOD 2018 – The 10th International Conference on Machine And Industrial Design In Mechanical Engineering (2018):136-137,
https://hdl.handle.net/21.15107/rcub_machinery_7592 .

Dynamic stability of high speed turboshaft engine with reducer

Kolarević, Nenad; Micković, D.; Crnojević, Stevan; Stanković, Miloš; Ognjanović, Milosav; Miloš, Marko

(Institute of Physics Publishing, 2018)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Micković, D.
AU  - Crnojević, Stevan
AU  - Stanković, Miloš
AU  - Ognjanović, Milosav
AU  - Miloš, Marko
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2979
AB  - The dynamic behavior of machines which rotate at extreme high speeds is crucial for stable and long operation. In design process some dynamics calculation must be taken into account to avoid potential operation near resonance areas. This paper considers dynamic analysis of the high speed reducer, designed together with the turbo-shaft engine. Resonances can occur when frequency of rotation and teeth mesh frequency are close to gear pair in mesh natural frequency, to the shafts natural frequencies and to the other parts natural frequencies. Problems can be avoided by translating resonant areas to higher or lower level of frequency by changing some design parameters, mass, stiffness and by variation of the stiffness of bearing supports. The paper presents the approaches to natural frequencies identification for the example of high speed reducer design. Some examples of design solutions, especially for elastic bearing supports and their experimental testing are also presented.
PB  - Institute of Physics Publishing
C3  - IOP Conference Series: Materials Science and Engineering
T1  - Dynamic stability of high speed turboshaft engine with reducer
IS  - 1
VL  - 393
DO  - 10.1088/1757-899X/393/1/012070
ER  - 
@conference{
author = "Kolarević, Nenad and Micković, D. and Crnojević, Stevan and Stanković, Miloš and Ognjanović, Milosav and Miloš, Marko",
year = "2018",
abstract = "The dynamic behavior of machines which rotate at extreme high speeds is crucial for stable and long operation. In design process some dynamics calculation must be taken into account to avoid potential operation near resonance areas. This paper considers dynamic analysis of the high speed reducer, designed together with the turbo-shaft engine. Resonances can occur when frequency of rotation and teeth mesh frequency are close to gear pair in mesh natural frequency, to the shafts natural frequencies and to the other parts natural frequencies. Problems can be avoided by translating resonant areas to higher or lower level of frequency by changing some design parameters, mass, stiffness and by variation of the stiffness of bearing supports. The paper presents the approaches to natural frequencies identification for the example of high speed reducer design. Some examples of design solutions, especially for elastic bearing supports and their experimental testing are also presented.",
publisher = "Institute of Physics Publishing",
journal = "IOP Conference Series: Materials Science and Engineering",
title = "Dynamic stability of high speed turboshaft engine with reducer",
number = "1",
volume = "393",
doi = "10.1088/1757-899X/393/1/012070"
}
Kolarević, N., Micković, D., Crnojević, S., Stanković, M., Ognjanović, M.,& Miloš, M.. (2018). Dynamic stability of high speed turboshaft engine with reducer. in IOP Conference Series: Materials Science and Engineering
Institute of Physics Publishing., 393(1).
https://doi.org/10.1088/1757-899X/393/1/012070
Kolarević N, Micković D, Crnojević S, Stanković M, Ognjanović M, Miloš M. Dynamic stability of high speed turboshaft engine with reducer. in IOP Conference Series: Materials Science and Engineering. 2018;393(1).
doi:10.1088/1757-899X/393/1/012070 .
Kolarević, Nenad, Micković, D., Crnojević, Stevan, Stanković, Miloš, Ognjanović, Milosav, Miloš, Marko, "Dynamic stability of high speed turboshaft engine with reducer" in IOP Conference Series: Materials Science and Engineering, 393, no. 1 (2018),
https://doi.org/10.1088/1757-899X/393/1/012070 . .
2

Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation

Kolarević, Nenad; Ognjanović, Milosav; Miloš, Marko

(Pergamon-Elsevier Science Ltd, Oxford, 2018)

TY  - JOUR
AU  - Kolarević, Nenad
AU  - Ognjanović, Milosav
AU  - Miloš, Marko
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2882
AB  - The multifunctional bulkhead is an assembly which divides the compressor and turbine space (cold and very hot area) in the gas-generator for turbo-jet and turbo-haft engines. The loads of this bulkhead present an interaction of mechanical, thermal, fluid stream and pressure effects which produce extreme operating conditions and specific kinds of failures. Additional unfavorable effects produce a high gradient and a variation of these loads. The article contains a numerical identification of bulkhead operating conditions and an innovative design of the bulkhead for this purpose. Design development is based on the specific failures which are analyzed together with causes and design possibilities for failure prevention. For this purpose, in the existing design approach "Property-based Design", a specific procedure named Failure-based design - FBD is applied. The paper also includes CFD analysis, numerical analyses of temperature, stress and deflection distribution of the multifunctional bulkhead. The presentation of the test stand and results of gas-generator testing together with the design solution of the multifunctional bulkhead, are also part of the article.
PB  - Pergamon-Elsevier Science Ltd, Oxford
T2  - Engineering Failure Analysis
T1  - Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation
EP  - 117
SP  - 100
VL  - 89
DO  - 10.1016/j.engfailanal.2018.02.022
ER  - 
@article{
author = "Kolarević, Nenad and Ognjanović, Milosav and Miloš, Marko",
year = "2018",
abstract = "The multifunctional bulkhead is an assembly which divides the compressor and turbine space (cold and very hot area) in the gas-generator for turbo-jet and turbo-haft engines. The loads of this bulkhead present an interaction of mechanical, thermal, fluid stream and pressure effects which produce extreme operating conditions and specific kinds of failures. Additional unfavorable effects produce a high gradient and a variation of these loads. The article contains a numerical identification of bulkhead operating conditions and an innovative design of the bulkhead for this purpose. Design development is based on the specific failures which are analyzed together with causes and design possibilities for failure prevention. For this purpose, in the existing design approach "Property-based Design", a specific procedure named Failure-based design - FBD is applied. The paper also includes CFD analysis, numerical analyses of temperature, stress and deflection distribution of the multifunctional bulkhead. The presentation of the test stand and results of gas-generator testing together with the design solution of the multifunctional bulkhead, are also part of the article.",
publisher = "Pergamon-Elsevier Science Ltd, Oxford",
journal = "Engineering Failure Analysis",
title = "Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation",
pages = "117-100",
volume = "89",
doi = "10.1016/j.engfailanal.2018.02.022"
}
Kolarević, N., Ognjanović, M.,& Miloš, M.. (2018). Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation. in Engineering Failure Analysis
Pergamon-Elsevier Science Ltd, Oxford., 89, 100-117.
https://doi.org/10.1016/j.engfailanal.2018.02.022
Kolarević N, Ognjanović M, Miloš M. Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation. in Engineering Failure Analysis. 2018;89:100-117.
doi:10.1016/j.engfailanal.2018.02.022 .
Kolarević, Nenad, Ognjanović, Milosav, Miloš, Marko, "Failures of multifunctional bulkhead caused by high gradient of temperature, pressure and speed of rotation" in Engineering Failure Analysis, 89 (2018):100-117,
https://doi.org/10.1016/j.engfailanal.2018.02.022 . .
4
2
5

Crucial parameters of gas generator on tip-jet helicopter

Kolarević, Nenad; Kosanović, N.; Miloš, Marko

(Elsevier Ltd, 2018)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Kosanović, N.
AU  - Miloš, Marko
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2843
AB  - The paper defines the minimum number of parameters which are sufficient for monitoring and controlling the gas generator operation in an innovative design of a tip-jet helicopter propulsion system. Firstly, the gas generator is tested separately on its test stand installation with several selected measuring and controlling parameters. Some ideas for implementing sensors for measuring certain parameters are presented in the paper. Then, a few parameters are selected as sufficient for controlling the tip-jet helicopter and experimentally verified on a helicopter hovering test as the minimum required parameters.
PB  - Elsevier Ltd
C3  - Materials Today: Proceedings
T1  - Crucial parameters of gas generator on tip-jet helicopter
EP  - 26720
IS  - 13
SP  - 26715
VL  - 5
DO  - 10.1016/j.matpr.2018.08.141
ER  - 
@conference{
author = "Kolarević, Nenad and Kosanović, N. and Miloš, Marko",
year = "2018",
abstract = "The paper defines the minimum number of parameters which are sufficient for monitoring and controlling the gas generator operation in an innovative design of a tip-jet helicopter propulsion system. Firstly, the gas generator is tested separately on its test stand installation with several selected measuring and controlling parameters. Some ideas for implementing sensors for measuring certain parameters are presented in the paper. Then, a few parameters are selected as sufficient for controlling the tip-jet helicopter and experimentally verified on a helicopter hovering test as the minimum required parameters.",
publisher = "Elsevier Ltd",
journal = "Materials Today: Proceedings",
title = "Crucial parameters of gas generator on tip-jet helicopter",
pages = "26720-26715",
number = "13",
volume = "5",
doi = "10.1016/j.matpr.2018.08.141"
}
Kolarević, N., Kosanović, N.,& Miloš, M.. (2018). Crucial parameters of gas generator on tip-jet helicopter. in Materials Today: Proceedings
Elsevier Ltd., 5(13), 26715-26720.
https://doi.org/10.1016/j.matpr.2018.08.141
Kolarević N, Kosanović N, Miloš M. Crucial parameters of gas generator on tip-jet helicopter. in Materials Today: Proceedings. 2018;5(13):26715-26720.
doi:10.1016/j.matpr.2018.08.141 .
Kolarević, Nenad, Kosanović, N., Miloš, Marko, "Crucial parameters of gas generator on tip-jet helicopter" in Materials Today: Proceedings, 5, no. 13 (2018):26715-26720,
https://doi.org/10.1016/j.matpr.2018.08.141 . .
2
2

Heat transfer and lubrication of turboshaft motor-reducer

Ognjanović, Milosav; Stanković, Miloš; Kolarević, Nenad

(Institute of Physics Publishing, 2018)

TY  - CONF
AU  - Ognjanović, Milosav
AU  - Stanković, Miloš
AU  - Kolarević, Nenad
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2973
AB  - Turboshaft engines, as the rule, contains gear transmission unit - reducer and belong to the group of drive systems with the name motor-reducer. These are the compact and autonomous assemblies for various applications. In the case of turboshaft engine in combination with high speed reducer, arise the set of phenomenon which has to be solved. Majority of them are in relation to reducer protection of overheating and of gears and bearings failures. The article contains analysis of heat sources, heat transfer through design structure and heat taking out in order to maintain acceptable temperature level of reducer lubricant. Theoretical discussions are supported with various experimental results and testing procedures, including analytic calculations. The set of design solutions for reducer protection when reducer located in the area of hot gas flow, is the main content. The case study is innovative design of turboshaft motor-reducer with free turbine which provides flexible operation and compact design structure.
PB  - Institute of Physics Publishing
C3  - IOP Conference Series: Materials Science and Engineering
T1  - Heat transfer and lubrication of turboshaft motor-reducer
IS  - 1
VL  - 393
DO  - 10.1088/1757-899X/393/1/012045
ER  - 
@conference{
author = "Ognjanović, Milosav and Stanković, Miloš and Kolarević, Nenad",
year = "2018",
abstract = "Turboshaft engines, as the rule, contains gear transmission unit - reducer and belong to the group of drive systems with the name motor-reducer. These are the compact and autonomous assemblies for various applications. In the case of turboshaft engine in combination with high speed reducer, arise the set of phenomenon which has to be solved. Majority of them are in relation to reducer protection of overheating and of gears and bearings failures. The article contains analysis of heat sources, heat transfer through design structure and heat taking out in order to maintain acceptable temperature level of reducer lubricant. Theoretical discussions are supported with various experimental results and testing procedures, including analytic calculations. The set of design solutions for reducer protection when reducer located in the area of hot gas flow, is the main content. The case study is innovative design of turboshaft motor-reducer with free turbine which provides flexible operation and compact design structure.",
publisher = "Institute of Physics Publishing",
journal = "IOP Conference Series: Materials Science and Engineering",
title = "Heat transfer and lubrication of turboshaft motor-reducer",
number = "1",
volume = "393",
doi = "10.1088/1757-899X/393/1/012045"
}
Ognjanović, M., Stanković, M.,& Kolarević, N.. (2018). Heat transfer and lubrication of turboshaft motor-reducer. in IOP Conference Series: Materials Science and Engineering
Institute of Physics Publishing., 393(1).
https://doi.org/10.1088/1757-899X/393/1/012045
Ognjanović M, Stanković M, Kolarević N. Heat transfer and lubrication of turboshaft motor-reducer. in IOP Conference Series: Materials Science and Engineering. 2018;393(1).
doi:10.1088/1757-899X/393/1/012045 .
Ognjanović, Milosav, Stanković, Miloš, Kolarević, Nenad, "Heat transfer and lubrication of turboshaft motor-reducer" in IOP Conference Series: Materials Science and Engineering, 393, no. 1 (2018),
https://doi.org/10.1088/1757-899X/393/1/012045 . .

Measuring the axial force on turbo-jet engine rotor

Kolarević, Nenad; Stanković, Miloš; Crnojević, Stevan; Micković, D.; Miloš, Marko

(DANUBIA Adria Symposium on Advances in Experimental Mechanics, 2018)

TY  - CONF
AU  - Kolarević, Nenad
AU  - Stanković, Miloš
AU  - Crnojević, Stevan
AU  - Micković, D.
AU  - Miloš, Marko
PY  - 2018
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2953
PB  - DANUBIA Adria Symposium on Advances in Experimental Mechanics
C3  - 35th Danubia Adria Symposium on Advances in Experimental Mechanics
T1  - Measuring the axial force on turbo-jet engine rotor
EP  - 42
SP  - 41
UR  - https://hdl.handle.net/21.15107/rcub_machinery_2953
ER  - 
@conference{
author = "Kolarević, Nenad and Stanković, Miloš and Crnojević, Stevan and Micković, D. and Miloš, Marko",
year = "2018",
publisher = "DANUBIA Adria Symposium on Advances in Experimental Mechanics",
journal = "35th Danubia Adria Symposium on Advances in Experimental Mechanics",
title = "Measuring the axial force on turbo-jet engine rotor",
pages = "42-41",
url = "https://hdl.handle.net/21.15107/rcub_machinery_2953"
}
Kolarević, N., Stanković, M., Crnojević, S., Micković, D.,& Miloš, M.. (2018). Measuring the axial force on turbo-jet engine rotor. in 35th Danubia Adria Symposium on Advances in Experimental Mechanics
DANUBIA Adria Symposium on Advances in Experimental Mechanics., 41-42.
https://hdl.handle.net/21.15107/rcub_machinery_2953
Kolarević N, Stanković M, Crnojević S, Micković D, Miloš M. Measuring the axial force on turbo-jet engine rotor. in 35th Danubia Adria Symposium on Advances in Experimental Mechanics. 2018;:41-42.
https://hdl.handle.net/21.15107/rcub_machinery_2953 .
Kolarević, Nenad, Stanković, Miloš, Crnojević, Stevan, Micković, D., Miloš, Marko, "Measuring the axial force on turbo-jet engine rotor" in 35th Danubia Adria Symposium on Advances in Experimental Mechanics (2018):41-42,
https://hdl.handle.net/21.15107/rcub_machinery_2953 .