Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC)
Апстракт
This paper introduces a new physical model of the gas flow through the 2D nozzle with the tilted obstacle in exit section. Experimental research on the 2D full span model in the supersonic indraft tunnel, which includes over three hundred tunnel runs, are presented. Variable geometric parameters were: nozzle shadow area, obstacle-nozzle wall angle, obstacle-nozzle gap and nozzle area ratio. In its conclusion, the paper discusses results and presents some suggestions for the future research.
Кључне речи:
Thrust / Thrust vector control / Schlieren photo / Pressure distribution / Mechanical obstacle / Gas flow / 2D nozzleИзвор:
Strojarstvo, 2011, 53, 4, 287-292Издавач:
- Croation Union of Mech. Engineers and Naval Architects
Колекције
Институција/група
Mašinski fakultetTY - JOUR AU - Stefanović, Zoran AU - Miloš, Marko AU - Todić, Ivana AU - Pavlović, M. PY - 2011 UR - https://machinery.mas.bg.ac.rs/handle/123456789/1331 AB - This paper introduces a new physical model of the gas flow through the 2D nozzle with the tilted obstacle in exit section. Experimental research on the 2D full span model in the supersonic indraft tunnel, which includes over three hundred tunnel runs, are presented. Variable geometric parameters were: nozzle shadow area, obstacle-nozzle wall angle, obstacle-nozzle gap and nozzle area ratio. In its conclusion, the paper discusses results and presents some suggestions for the future research. PB - Croation Union of Mech. Engineers and Naval Architects T2 - Strojarstvo T1 - Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC) EP - 292 IS - 4 SP - 287 VL - 53 UR - https://hdl.handle.net/21.15107/rcub_machinery_1331 ER -
@article{ author = "Stefanović, Zoran and Miloš, Marko and Todić, Ivana and Pavlović, M.", year = "2011", abstract = "This paper introduces a new physical model of the gas flow through the 2D nozzle with the tilted obstacle in exit section. Experimental research on the 2D full span model in the supersonic indraft tunnel, which includes over three hundred tunnel runs, are presented. Variable geometric parameters were: nozzle shadow area, obstacle-nozzle wall angle, obstacle-nozzle gap and nozzle area ratio. In its conclusion, the paper discusses results and presents some suggestions for the future research.", publisher = "Croation Union of Mech. Engineers and Naval Architects", journal = "Strojarstvo", title = "Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC)", pages = "292-287", number = "4", volume = "53", url = "https://hdl.handle.net/21.15107/rcub_machinery_1331" }
Stefanović, Z., Miloš, M., Todić, I.,& Pavlović, M.. (2011). Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC). in Strojarstvo Croation Union of Mech. Engineers and Naval Architects., 53(4), 287-292. https://hdl.handle.net/21.15107/rcub_machinery_1331
Stefanović Z, Miloš M, Todić I, Pavlović M. Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC). in Strojarstvo. 2011;53(4):287-292. https://hdl.handle.net/21.15107/rcub_machinery_1331 .
Stefanović, Zoran, Miloš, Marko, Todić, Ivana, Pavlović, M., "Investigation of the pressure distribution in a 2D rocket nozzle with a mechanical system for thrust vector control (TVC)" in Strojarstvo, 53, no. 4 (2011):287-292, https://hdl.handle.net/21.15107/rcub_machinery_1331 .