Profiling of a Supersonic Combustion Chamber and Nozzle Under Constraints on the Total Length

1998 ◽  
Vol 33 (5) ◽  
pp. 637-644 ◽  
Author(s):  
A. N. Kraiko ◽  
V. E. Makarov ◽  
N. I. Tillyayeya
Keyword(s):  
Combustion Chamber ◽  
Supersonic Combustion ◽  
Total Length

scholarly journals Characteristics of gaseous film cooling with hydrocarbon fuel in supersonic combustion chamber

2021 ◽  
Author(s):  
Tingting Jing ◽  
Zhen Xu ◽  
Jiachen Xu ◽  
Fei Qin ◽  
Guoqiang He ◽  
...  
Keyword(s):  
Combustion Chamber ◽  
Film Cooling ◽  
Hydrocarbon Fuel ◽  
Supersonic Combustion

Computational investigation of multi-cavity fuel injection on hydrogen mixing at supersonic combustion chamber

2020 ◽  
Vol 45 (15) ◽  
pp. 9077-9087 ◽  
Author(s):  
Zhixiong Li ◽  
Tran Dinh Manh ◽  
M. Barzegar Gerdroodbary ◽  
Nguyen Dang Nam ◽  
R. Moradi ◽  
...  
Keyword(s):  
Combustion Chamber ◽  
Fuel Injection ◽  
Supersonic Combustion ◽  
Computational Investigation

Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber

2020 ◽  
Vol 45 (51) ◽  
pp. 27828-27836 ◽  
Author(s):  
Yu Jiang ◽  
Amin Poozesh ◽  
Seyed Maziar Marashi ◽  
R. Moradi ◽  
M. Barzegar Gerdroodbary ◽  
...  
Keyword(s):  
Combustion Chamber ◽  
Supersonic Combustion ◽  
Mixing Efficiency

Design of a Focusing Schlieren Setup for Use in a Supersonic Combustion Chamber

2017 ◽  
pp. 1467-1471 ◽  
Author(s):  
Manuel N. Bühler ◽  
Felix J. Förster ◽  
Nils C. Dröske ◽  
Jens von Wolfersdorf ◽  
Bernhard Weigand
Keyword(s):  
Combustion Chamber ◽  
Supersonic Combustion

Inlet air and fuel flow pressure fluctuation effect on supersonic combustion

2020 ◽  
Vol ahead-of-print (ahead-of-print) ◽  
Author(s):  
AmirMahdi Tahsini
Keyword(s):  
Shock Wave ◽  
Combustion Chamber ◽  
Pressure Fluctuations ◽  
Combustion Efficiency ◽  
Supersonic Combustion ◽  
Oblique Shock Wave ◽  
Reacting Flow ◽  
Content Type ◽  
Fuel Flow ◽  
Flow Stream

Purpose The purpose of this paper is to analyze the effect of pressure fluctuations on the combustion efficiency of the hydrogen fuel injected into the supersonic oxidizing cross flow. The pressure fluctuations are imposed on inlet air flow and also on the fuel flow stream. Two different situations are considered: the combustion chamber once without and again with the inlet standing oblique shock wave. Design/methodology/approach The pressure fluctuations are imposed on inlet air flow and also on the fuel flow stream. Two different situations are considered: the combustion chamber once without and again with the inlet standing oblique shock wave. The unsteady turbulent reacting flow solver is developed to simulate the supersonic flow field in the combustion chamber with detail chemical kinetics, to predict the time-variation of the combustion efficiency due to the imposed pressure fluctuations. Findings The results show that the response of the reacting flow field depends on both the frequency of fluctuations and the existence of the inlet shock wave. In addition, the inlet standing shock wave has some attenuating role, but the reacting flow shows an amplifying role on imposed oscillations which is also augmented by imposing anti-phase fluctuations on both inlet and fuel flow streams. Originality/value This study is performed to analyze the instabilities in the supersonic combustion which has not been considered before in this manner.

Effect of free stream angle on mixing performance of hydrogen multi-jets in supersonic combustion chamber

2020 ◽  
Vol 45 (46) ◽  
pp. 25426-25437 ◽  
Author(s):  
Yu Jiang ◽  
M. Barzegar Gerdroodbary ◽  
M. Sheikholeslami ◽  
Houman Babazadeh ◽  
Ahmad Shafee ◽  
...  
Keyword(s):  
Combustion Chamber ◽  
Free Stream ◽  
Supersonic Combustion ◽  
Mixing Performance

Comparison of different lobe-injectors on fuel mixing characteristics of single jet at the supersonic combustion chamber

2021 ◽  
pp. 107193
Author(s):  
Guangli Fan ◽  
Hassan Abdulwahab Anjal ◽  
Raed Qahiti ◽  
Nidal H. Abu-Hamdeh ◽  
Abdullah M. Abusorrah ◽  
...  
Keyword(s):  
Combustion Chamber ◽  
Supersonic Combustion ◽  
Mixing Characteristics ◽  
Single Jet ◽  
Fuel Mixing

Flow Field Characteristics of Butterfly-Type Cavity and its Influence on Supersonic Flow

2011 ◽  
Vol 347-353 ◽  
pp. 2468-2474
Author(s):  
Jin Xiang Wu ◽  
Jing Ma ◽  
Xiang Gou ◽  
Lian Sheng Liu ◽  
En Yu Wang
Keyword(s):  
Energy Dissipation ◽  
Kinetic Energy ◽  
Combustion Chamber ◽  
Turbulent Kinetic Energy ◽  
Energy Dissipation Rate ◽  
Hydrogen Gas ◽  
Supersonic Combustion ◽  
Flow Field Characteristics ◽  
Cavity Configuration ◽  
New Type

A new type of cavity configuration — butterfly-type cavity applied in the scramjet is proposed in this paper. The supersonic combustion chamber with Butterfly-type cavity was investigated numerically and experimentally. Results show that the horizontal vortex moving along the Y direction is helpful in gathering hydrogen gas, but the vertical vortex moving along the Z direction is not. Both turbulent kinetic energy and turbulent kinetic energy dissipation rate are very high at the junction between the cavity and the main combustion chamber. And the production of turbulent kinetic energy is agreeable with that of turbulent kinetic energy dissipation.

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