The radiation field of a hypersonic nozzle flow

1977 ◽  
Vol 18 (4) ◽  
pp. 385-389
Author(s):  
P.F. Logan ◽  
R.J. Stalker
AIAA Journal ◽  
1964 ◽  
Vol 2 (1) ◽  
pp. 148-150 ◽  
Author(s):  
M. SICHEL

AIAA Journal ◽  
2018 ◽  
Vol 56 (7) ◽  
pp. 2930-2935
Author(s):  
Yedhu Krishna ◽  
Suzanne L. Sheehe ◽  
Sean O’Byrne

Shock Waves ◽  
2006 ◽  
Vol 15 (2) ◽  
pp. 81-87 ◽  
Author(s):  
S. O’Byrne ◽  
P. M. Danehy ◽  
A. F. P. Houwing

1973 ◽  
Vol 58 (4) ◽  
pp. 749-761 ◽  
Author(s):  
R. J. Stalker ◽  
M. K. McIntosh

An experimental investigation was undertaken of the flow produced by the inviscid expansion of air through a hypersonic nozzle. Stagnation enthalpy levels up to 4 × 107J/kg were used, with initial dissociation levels approaching 90%. By measuring the flow velocity and the frozen dissociation fractions of oxygen and nitrogen, it was found that existing theoretical models served adequately to define the nozzle flow, at least for the purpose of conducting experiments involving reacting inviscid hypersonic flows about blunt bodies.


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

Sign in / Sign up

Export Citation Format

Share Document