TY  - JOUR
AU  - Živković, Saša Ž.
AU  - Milinović, Momčilo M.
AU  - Stefanović, Predrag Lj.
AU  - Pavlović, Pavle B.
AU  - Gligorijević, Nikola I.
PY  - 2016
UR  - https://vinar.vin.bg.ac.rs/handle/123456789/1150
AB  - The paper discusses the temperature changes in mechanical jet tabs in a system of rocket motor thrust vector control, estimated by the simulation and experimental tests methodology. The heat transfer calculation is based on complex computational fluid dynamics simulations of both the nozzle and external tab flows, as the comprehensive integral flow zones with high flow parameters gradients. Due to a complexity of the model for flow calculations, the experimental estimation of the calculated results is carried out. The temperature is measured by jet tabs embedded thermocouples, and conducted through the rocket motor static tests. A good agreement of the calculated and measured results is achieved. The main aim of the developed method is to establish an approved calculation tool for designing new thurst vector control systems in order to avoid disadvantages due to overheating.
T2  - Thermal Science
T1  - Experimental and Simulation Testing of Thermal Loading in the Jet Tabs of a Thrust Vector Control System
VL  - 20
SP  - S275
EP  - S286
DO  - 10.2298/TSCI150914208Z
ER  - 

@article{
author = "Živković, Saša Ž. and Milinović, Momčilo M. and Stefanović, Predrag Lj. and Pavlović, Pavle B. and Gligorijević, Nikola I.",
year = "2016",
abstract = "The paper discusses the temperature changes in mechanical jet tabs in a system of rocket motor thrust vector control, estimated by the simulation and experimental tests methodology. The heat transfer calculation is based on complex computational fluid dynamics simulations of both the nozzle and external tab flows, as the comprehensive integral flow zones with high flow parameters gradients. Due to a complexity of the model for flow calculations, the experimental estimation of the calculated results is carried out. The temperature is measured by jet tabs embedded thermocouples, and conducted through the rocket motor static tests. A good agreement of the calculated and measured results is achieved. The main aim of the developed method is to establish an approved calculation tool for designing new thurst vector control systems in order to avoid disadvantages due to overheating.",
journal = "Thermal Science",
title = "Experimental and Simulation Testing of Thermal Loading in the Jet Tabs of a Thrust Vector Control System",
volume = "20",
pages = "S275-S286",
doi = "10.2298/TSCI150914208Z"
}

Živković, S. Ž., Milinović, M. M., Stefanović, P. Lj., Pavlović, P. B.,& Gligorijević, N. I.. (2016). Experimental and Simulation Testing of Thermal Loading in the Jet Tabs of a Thrust Vector Control System. in Thermal Science, 20, S275-S286.
https://doi.org/10.2298/TSCI150914208Z

Živković SŽ, Milinović MM, Stefanović PL, Pavlović PB, Gligorijević NI. Experimental and Simulation Testing of Thermal Loading in the Jet Tabs of a Thrust Vector Control System. in Thermal Science. 2016;20:S275-S286.
doi:10.2298/TSCI150914208Z .

Živković, Saša Ž., Milinović, Momčilo M., Stefanović, Predrag Lj., Pavlović, Pavle B., Gligorijević, Nikola I., "Experimental and Simulation Testing of Thermal Loading in the Jet Tabs of a Thrust Vector Control System" in Thermal Science, 20 (2016):S275-S286,
https://doi.org/10.2298/TSCI150914208Z . .