Low cost space transportation systems

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Low cost space transportation systems (en)
Космички транспортни системи ниске цене (sr)
Kosmički transportni sistemi niske cene (sr_RS)
Authors

Publications

Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures

Elmiladi, Abdulrazag Abdallah; Petrović, Veljko M.; Grbović, Aleksandar; Sedmak, Aleksandar; Balać, Igor

(Univerzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd, 2021)

TY  - JOUR
AU  - Elmiladi, Abdulrazag Abdallah
AU  - Petrović, Veljko M.
AU  - Grbović, Aleksandar
AU  - Sedmak, Aleksandar
AU  - Balać, Igor
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3524
AB  - This paper presents numerical calculation of thermal stresses generated in a carbon fiber-epoxy laminated composite structure which is operating at low temperatures. The thermal stress evaluation is based on the finite element method. A sample problem involving generated thermal stresses in a real laminated composite structure, exposed to low temperatures (four different temperature levels), is analyzed and discussed. Obtained results suggest that these thermal stresses remarkably decrease the strength of the laminated composite structure.
PB  - Univerzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd
T2  - Thermal Science
T1  - Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures
EP  - 3856
IS  - 5
SP  - 3847
VL  - 25
DO  - 10.2298/TSCI200729338E
ER  - 
@article{
author = "Elmiladi, Abdulrazag Abdallah and Petrović, Veljko M. and Grbović, Aleksandar and Sedmak, Aleksandar and Balać, Igor",
year = "2021",
abstract = "This paper presents numerical calculation of thermal stresses generated in a carbon fiber-epoxy laminated composite structure which is operating at low temperatures. The thermal stress evaluation is based on the finite element method. A sample problem involving generated thermal stresses in a real laminated composite structure, exposed to low temperatures (four different temperature levels), is analyzed and discussed. Obtained results suggest that these thermal stresses remarkably decrease the strength of the laminated composite structure.",
publisher = "Univerzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd",
journal = "Thermal Science",
title = "Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures",
pages = "3856-3847",
number = "5",
volume = "25",
doi = "10.2298/TSCI200729338E"
}
Elmiladi, A. A., Petrović, V. M., Grbović, A., Sedmak, A.,& Balać, I.. (2021). Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures. in Thermal Science
Univerzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd., 25(5), 3847-3856.
https://doi.org/10.2298/TSCI200729338E
Elmiladi AA, Petrović VM, Grbović A, Sedmak A, Balać I. Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures. in Thermal Science. 2021;25(5):3847-3856.
doi:10.2298/TSCI200729338E .
Elmiladi, Abdulrazag Abdallah, Petrović, Veljko M., Grbović, Aleksandar, Sedmak, Aleksandar, Balać, Igor, "Numerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperatures" in Thermal Science, 25, no. 5 (2021):3847-3856,
https://doi.org/10.2298/TSCI200729338E . .
2
3

A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models

Sekutkovski, Bojan; Grbović, Aleksandar; Todić, Ivana; Pejčev, Aleksandar

(Elsevier France-Editions Scientifiques Medicales Elsevier, Issy-Les-Moulineaux, 2021)

TY  - JOUR
AU  - Sekutkovski, Bojan
AU  - Grbović, Aleksandar
AU  - Todić, Ivana
AU  - Pejčev, Aleksandar
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3562
AB  - In this work the partitioned solution approach for the fluid-structure interaction (FSI) of thin-walled structures and high-Reynolds number (Re) flows modeled using Reynolds-Averaged Navier-Stokes (RANS) and hybrid Reynolds-Averaged Navier-Stokes - Large Eddy Simulation (RANS-LES) turbulence models are described. The advanced turbulence modeling is needed to capture very complex fluid phenomena which triggers instabilities of thin-walled structures present in supersonic flow regimes. The finite element (FE) updated Lagrangian formulation (ULF) for the nonlinear elastic solids is used to predict its dynamical behavior. The main contribution addresses to the linear stress-strain relation Laplacian members, which are solved implicitly, on that way decreasing required memory resources and improving solution stability in the same time. The structures of the interest include the vast variety of membranes, curved shells and plates. The instabilities encountering these structures include limit cycle oscillations (LCO), flutter and buckling of the panels. The phenomena appear in everyday engineering practice and a need for the powerful tools to handle such problems is a common goal. Utilization of the unstructured non-regular meshes allows the precise distribution of computational nodes at the physical boundaries of the fluid and solid domains. It is naturally allowing application of the common approach for the fluid-solid interface coupling, as well as classical data interpolation schemes between fluid and solid on the FSI interface. High-Re flows, both 2D (benchmark) and 3D turbulent FSI case are chosen for the validation. Two numerical methods are coupled via a moving boundary treatment, in a staggered way. The proposed coupling method showed a good agreement with the reference test cases. The current FSI framework is developed to serve as a tool for the liquid rocket engine development.
PB  - Elsevier France-Editions Scientifiques Medicales Elsevier, Issy-Les-Moulineaux
T2  - Aerospace Science and Technology
T1  - A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models
VL  - 113
DO  - 10.1016/j.ast.2021.106629
ER  - 
@article{
author = "Sekutkovski, Bojan and Grbović, Aleksandar and Todić, Ivana and Pejčev, Aleksandar",
year = "2021",
abstract = "In this work the partitioned solution approach for the fluid-structure interaction (FSI) of thin-walled structures and high-Reynolds number (Re) flows modeled using Reynolds-Averaged Navier-Stokes (RANS) and hybrid Reynolds-Averaged Navier-Stokes - Large Eddy Simulation (RANS-LES) turbulence models are described. The advanced turbulence modeling is needed to capture very complex fluid phenomena which triggers instabilities of thin-walled structures present in supersonic flow regimes. The finite element (FE) updated Lagrangian formulation (ULF) for the nonlinear elastic solids is used to predict its dynamical behavior. The main contribution addresses to the linear stress-strain relation Laplacian members, which are solved implicitly, on that way decreasing required memory resources and improving solution stability in the same time. The structures of the interest include the vast variety of membranes, curved shells and plates. The instabilities encountering these structures include limit cycle oscillations (LCO), flutter and buckling of the panels. The phenomena appear in everyday engineering practice and a need for the powerful tools to handle such problems is a common goal. Utilization of the unstructured non-regular meshes allows the precise distribution of computational nodes at the physical boundaries of the fluid and solid domains. It is naturally allowing application of the common approach for the fluid-solid interface coupling, as well as classical data interpolation schemes between fluid and solid on the FSI interface. High-Re flows, both 2D (benchmark) and 3D turbulent FSI case are chosen for the validation. Two numerical methods are coupled via a moving boundary treatment, in a staggered way. The proposed coupling method showed a good agreement with the reference test cases. The current FSI framework is developed to serve as a tool for the liquid rocket engine development.",
publisher = "Elsevier France-Editions Scientifiques Medicales Elsevier, Issy-Les-Moulineaux",
journal = "Aerospace Science and Technology",
title = "A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models",
volume = "113",
doi = "10.1016/j.ast.2021.106629"
}
Sekutkovski, B., Grbović, A., Todić, I.,& Pejčev, A.. (2021). A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models. in Aerospace Science and Technology
Elsevier France-Editions Scientifiques Medicales Elsevier, Issy-Les-Moulineaux., 113.
https://doi.org/10.1016/j.ast.2021.106629
Sekutkovski B, Grbović A, Todić I, Pejčev A. A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models. in Aerospace Science and Technology. 2021;113.
doi:10.1016/j.ast.2021.106629 .
Sekutkovski, Bojan, Grbović, Aleksandar, Todić, Ivana, Pejčev, Aleksandar, "A partitioned solution approach for the fluid-structure interaction of thin-walled structures and high-Reynolds number flows using RANS and hybrid RANS-LES turbulence models" in Aerospace Science and Technology, 113 (2021),
https://doi.org/10.1016/j.ast.2021.106629 . .
3
4

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 .

A novel 6 dof thrust vector control test stand

Miloš, Predrag; Davidović, Nikola; Jojić, Branislav; Miloš, Marko; Todić, Ivana

(Univ Osijek, Tech Fac, Slavonski Brod, 2015)

TY  - JOUR
AU  - Miloš, Predrag
AU  - Davidović, Nikola
AU  - Jojić, Branislav
AU  - Miloš, Marko
AU  - Todić, Ivana
PY  - 2015
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2228
AB  - This study proposes an innovative test stand design to accurately measure rocket motor thrust vector during its operation. Test stand design is clearly presented as well as procedure and mathematical model for its calibration. A method of processing data obtained from the experiments and the results of the jet tab system for thrust vector control are presented in detail. Experiments have shown that the test stand is highly functional and the results obtained have excellent repeatability and matching with the results of the other authors who have used different construction test stands for measurement of the same or a similar mechanism for thrust vector control.
PB  - Univ Osijek, Tech Fac, Slavonski Brod
T2  - Tehnički vjesnik
T1  - A novel 6 dof thrust vector control test stand
EP  - 1254
IS  - 5
SP  - 1247
VL  - 22
DO  - 10.17559/TV-20140621064603
ER  - 
@article{
author = "Miloš, Predrag and Davidović, Nikola and Jojić, Branislav and Miloš, Marko and Todić, Ivana",
year = "2015",
abstract = "This study proposes an innovative test stand design to accurately measure rocket motor thrust vector during its operation. Test stand design is clearly presented as well as procedure and mathematical model for its calibration. A method of processing data obtained from the experiments and the results of the jet tab system for thrust vector control are presented in detail. Experiments have shown that the test stand is highly functional and the results obtained have excellent repeatability and matching with the results of the other authors who have used different construction test stands for measurement of the same or a similar mechanism for thrust vector control.",
publisher = "Univ Osijek, Tech Fac, Slavonski Brod",
journal = "Tehnički vjesnik",
title = "A novel 6 dof thrust vector control test stand",
pages = "1254-1247",
number = "5",
volume = "22",
doi = "10.17559/TV-20140621064603"
}
Miloš, P., Davidović, N., Jojić, B., Miloš, M.,& Todić, I.. (2015). A novel 6 dof thrust vector control test stand. in Tehnički vjesnik
Univ Osijek, Tech Fac, Slavonski Brod., 22(5), 1247-1254.
https://doi.org/10.17559/TV-20140621064603
Miloš P, Davidović N, Jojić B, Miloš M, Todić I. A novel 6 dof thrust vector control test stand. in Tehnički vjesnik. 2015;22(5):1247-1254.
doi:10.17559/TV-20140621064603 .
Miloš, Predrag, Davidović, Nikola, Jojić, Branislav, Miloš, Marko, Todić, Ivana, "A novel 6 dof thrust vector control test stand" in Tehnički vjesnik, 22, no. 5 (2015):1247-1254,
https://doi.org/10.17559/TV-20140621064603 . .
7
2
7

Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion

Davidović, Nikola; Miloš, Predrag; Jojić, Branislav; Miloš, Marko

(Univ Osijek, Tech Fac, Slavonski Brod, 2015)

TY  - JOUR
AU  - Davidović, Nikola
AU  - Miloš, Predrag
AU  - Jojić, Branislav
AU  - Miloš, Marko
PY  - 2015
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2257
AB  - Physical model of spoiler and dome deflector thrust vector control (TVC) system was established considering previous and current research observations. According to logic of physical model an engineering mathematical model is derived. Model algorithm and results were analysed and explained. Finally, model data were confirmed with real motor tests.
PB  - Univ Osijek, Tech Fac, Slavonski Brod
T2  - Tehnički vjesnik
T1  - Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion
EP  - 915
IS  - 4
SP  - 907
VL  - 22
DO  - 10.17559/TV-20140621063849
ER  - 
@article{
author = "Davidović, Nikola and Miloš, Predrag and Jojić, Branislav and Miloš, Marko",
year = "2015",
abstract = "Physical model of spoiler and dome deflector thrust vector control (TVC) system was established considering previous and current research observations. According to logic of physical model an engineering mathematical model is derived. Model algorithm and results were analysed and explained. Finally, model data were confirmed with real motor tests.",
publisher = "Univ Osijek, Tech Fac, Slavonski Brod",
journal = "Tehnički vjesnik",
title = "Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion",
pages = "915-907",
number = "4",
volume = "22",
doi = "10.17559/TV-20140621063849"
}
Davidović, N., Miloš, P., Jojić, B.,& Miloš, M.. (2015). Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion. in Tehnički vjesnik
Univ Osijek, Tech Fac, Slavonski Brod., 22(4), 907-915.
https://doi.org/10.17559/TV-20140621063849
Davidović N, Miloš P, Jojić B, Miloš M. Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion. in Tehnički vjesnik. 2015;22(4):907-915.
doi:10.17559/TV-20140621063849 .
Davidović, Nikola, Miloš, Predrag, Jojić, Branislav, Miloš, Marko, "Contribution to research of spoiler and dome deflector tvc systems in rocket propulsion" in Tehnički vjesnik, 22, no. 4 (2015):907-915,
https://doi.org/10.17559/TV-20140621063849 . .
1
3

Different modeling technologies of hydraulic load simulator for thrust vector control actuator

Nauparac, Dragan B.; Prsić, Dragan H.; Miloš, Marko; Todić, Ivana

(Univ Osijek, Tech Fac, Slavonski Brod, 2015)

TY  - JOUR
AU  - Nauparac, Dragan B.
AU  - Prsić, Dragan H.
AU  - Miloš, Marko
AU  - Todić, Ivana
PY  - 2015
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/2191
AB  - Hydraulic simulators are extremely important in the flight control actuator system's verification process. Flexible nozzle has a number of specifics, comparing to other flight controls, because the load cannot be described, classically, by the hinge moment. Additionally, classical hydraulic simulator, in which the cylinder simulates the load, is not sufficient for performing a complete simulation of the real load. Building a mechanical pendulum, to which a hydraulic cylinder acts, and that rests on two elastic supports, enables simulation of additional phenomena that exist in flexible nozzle, but not in other control surfaces. Force from impulse that exists in reality, and which is impossible to be generated by standard hydraulic simulator, can be realized through the pendulum. This paper demonstrates that a simulator can be designed through modelling of the elastic load using bond graph, without a precise elaboration of direction of forces in elastic structure, just by observing, on energy level, the input of force in flexible structure over the point in which actuator force acts. Simulator with hydraulic cylinder is convenient to be used when there is a need for considering the risk of self-oscillation of flexible joint and nozzle, i.e. for defining the so-called notch filter. Then, the hydraulic cylinder of load simulator can generate the oscillation, frequency and amplitude that match this dynamic case of flexible nozzle actuator's load that is being reduced to its piston rod, without a risk of damaging the flexible structure that exists in the construction of a simulator with pendulum.
PB  - Univ Osijek, Tech Fac, Slavonski Brod
T2  - Tehnički vjesnik
T1  - Different modeling technologies of hydraulic load simulator for thrust vector control actuator
EP  - 606
IS  - 3
SP  - 599
VL  - 22
DO  - 10.17559/TV-20140621063240
ER  - 
@article{
author = "Nauparac, Dragan B. and Prsić, Dragan H. and Miloš, Marko and Todić, Ivana",
year = "2015",
abstract = "Hydraulic simulators are extremely important in the flight control actuator system's verification process. Flexible nozzle has a number of specifics, comparing to other flight controls, because the load cannot be described, classically, by the hinge moment. Additionally, classical hydraulic simulator, in which the cylinder simulates the load, is not sufficient for performing a complete simulation of the real load. Building a mechanical pendulum, to which a hydraulic cylinder acts, and that rests on two elastic supports, enables simulation of additional phenomena that exist in flexible nozzle, but not in other control surfaces. Force from impulse that exists in reality, and which is impossible to be generated by standard hydraulic simulator, can be realized through the pendulum. This paper demonstrates that a simulator can be designed through modelling of the elastic load using bond graph, without a precise elaboration of direction of forces in elastic structure, just by observing, on energy level, the input of force in flexible structure over the point in which actuator force acts. Simulator with hydraulic cylinder is convenient to be used when there is a need for considering the risk of self-oscillation of flexible joint and nozzle, i.e. for defining the so-called notch filter. Then, the hydraulic cylinder of load simulator can generate the oscillation, frequency and amplitude that match this dynamic case of flexible nozzle actuator's load that is being reduced to its piston rod, without a risk of damaging the flexible structure that exists in the construction of a simulator with pendulum.",
publisher = "Univ Osijek, Tech Fac, Slavonski Brod",
journal = "Tehnički vjesnik",
title = "Different modeling technologies of hydraulic load simulator for thrust vector control actuator",
pages = "606-599",
number = "3",
volume = "22",
doi = "10.17559/TV-20140621063240"
}
Nauparac, D. B., Prsić, D. H., Miloš, M.,& Todić, I.. (2015). Different modeling technologies of hydraulic load simulator for thrust vector control actuator. in Tehnički vjesnik
Univ Osijek, Tech Fac, Slavonski Brod., 22(3), 599-606.
https://doi.org/10.17559/TV-20140621063240
Nauparac DB, Prsić DH, Miloš M, Todić I. Different modeling technologies of hydraulic load simulator for thrust vector control actuator. in Tehnički vjesnik. 2015;22(3):599-606.
doi:10.17559/TV-20140621063240 .
Nauparac, Dragan B., Prsić, Dragan H., Miloš, Marko, Todić, Ivana, "Different modeling technologies of hydraulic load simulator for thrust vector control actuator" in Tehnički vjesnik, 22, no. 3 (2015):599-606,
https://doi.org/10.17559/TV-20140621063240 . .
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