ARCJET Fundamentals: Experiments and Non-Equilibrium Flow Modeling.

1996 ◽  
Author(s):  
Herman Krier ◽  
Rodney L. Burton ◽  
S. A. Bufton ◽  
T. W. Megli
2002 ◽  
Vol 1 (1) ◽  
pp. 26-34
Author(s):  
Hong-tao Zheng ◽  
Zhi-yong Tan ◽  
Hai-ou Sun ◽  
Chun-liang Zhou ◽  
Zhi-ming Li

2014 ◽  
Vol 490-491 ◽  
pp. 931-935
Author(s):  
Xiao Yuan Zhang ◽  
Li Zi Qin ◽  
Yu Liu

The chemical non-equilibrium flow of supersonic combustion ramjet (scramjet) nozzle is numerical simulated with different chemical kinetic models to research the effects on numerical results of the nozzle performance. The numerical results show that total temperature is increased due to the recombination of dissociation compositions and the combustion of the residual fuel. The effect of the combustion of the residual fuel is more obvious in this paper, and the effect to the performance of the nozzle is noticeable. The species of the compositions in the models influence the quantity of heat sending out when it get equilibrium, so the 9-species chemical kinetic models are more suitable in the simulation of the scramjet nozzle chemical non-equilibrium flows.


1999 ◽  
Author(s):  
Takahisa Tokunaga ◽  
Makoto Hiraoka ◽  
A. Hayashi ◽  
Yasushi Watanabe

1993 ◽  
Vol 99 (1-4) ◽  
pp. 103-111 ◽  
Author(s):  
V. D. Sharma ◽  
B. D. Pandey ◽  
R. R. Sharma

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