Influence of Starting Chamber Dynamics on Nozzle Flow Choking Time and the Liftoff Time of Dual-thrust Rockets

Author(s):  
Sivabalan Mani ◽  
R. Tharikaa ◽  
S. Ajith ◽  
N. Naveen ◽  
R. Vignesh ◽  
...  
Keyword(s):  
Author(s):  
VR Sanal Kumar ◽  
Chandrasekaran Nichith ◽  
S Vigneshwaran ◽  
Anbarasan S ◽  
Ashish Kumar ◽  
...  

2007 ◽  
Vol 17 (6) ◽  
pp. 529-550 ◽  
Author(s):  
Seoksu Moon ◽  
Choongsik Bae ◽  
Essam F. Abo-Serie ◽  
Jaejoon Choi

AIAA Journal ◽  
1998 ◽  
Vol 36 ◽  
pp. 349-358 ◽  
Author(s):  
S. C. M. Yu ◽  
X. G. Xu
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AIAA Journal ◽  
1998 ◽  
Vol 36 ◽  
pp. 1618-1625 ◽  
Author(s):  
G. L. Romine
Keyword(s):  

2000 ◽  
Author(s):  
N. Sijtsema ◽  
R. Tolboom ◽  
N. Dam ◽  
J. ter Meulen
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2017 ◽  
Vol 29 (6) ◽  
pp. 1035-1043 ◽  
Author(s):  
Zhao-xin Gong ◽  
Chuan-jing Lu ◽  
Jie Li ◽  
Jia-yi Cao

1960 ◽  
Vol 64 (598) ◽  
pp. 632-635 ◽  
Author(s):  
R. A. A. Bryant

The concept of small stage efficiency is introduced when studying one-dimensional gas flow in nozzles in order to permit a closer approximation of real flow conditions than is possible from an isentropic analysis. It is more or less conventional to assume the flow conditions are adiabatic whenever the small stage efficiency is used. That is to say, small stage efficiency is generally considered in relation to flows contained within adiabatic boundaries, in which case it becomes a measure of the heat generated by internal frictional effects alone.


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