An Attempted Improvement of the Method of Integral Relations for a Blunt Body in a Supersonic Flow

AIAA Journal ◽  
1973 ◽  
Vol 11 (11) ◽  
pp. 1575-1576
Author(s):  
B. L. HUNT
Keyword(s):  
Supersonic Flow ◽  
Blunt Body ◽  
Method Of Integral Relations ◽  
Integral Relations

Nonadiabatic Flow Around Blunt Bodies at Hyperbolic Speeds

1970 ◽  
Vol 37 (2) ◽  
pp. 461-466
Author(s):  
H. S. Bluston
Keyword(s):  
Shock Layer ◽  
Blunt Body ◽  
Energy Equation ◽  
Numerical Results ◽  
Temperature Profiles ◽  
Differential Approximation ◽  
Blunt Bodies ◽  
Method Of Integral Relations ◽  
Nonadiabatic Effects ◽  
Integral Relations

This investigation applies Belotserkovskii’s method of integral relations to the nonadiabatic, self-absorbing radiative flow of a gray gas about a sharp-cornered blunt body. The radiative quantities are represented by means of the “differential approximation.” Nonadiabatic effects are included both in the energy equation and in the shock layer temperature profiles. Numerical results are presented for flow about an Apollo-type capsule reentering the Earth’s atmosphere at an altitude of 190,000 ft and a velocity of 48,000 fps.

Nonequilibrium blunt-body flow using the method of integral relations

AIAA Journal ◽  
1964 ◽  
Vol 2 (6) ◽  
pp. 1062-1071 ◽  
Author(s):  
W. C. L. SHIH ◽  
J. R. BARON
Keyword(s):  
Blunt Body ◽  
Method Of Integral Relations ◽  
Integral Relations

Heat transfer at the nose of a blunt body in a rarefied supersonic flow of a nitrogen-hydrogen mixture

1975 ◽  
Vol 14 (6) ◽  
pp. 809-812 ◽  
Author(s):  
A. A. Bochkarev ◽  
V. A. Kosinov ◽  
V. G. Prikhod'ko ◽  
A. K. Rebrov
Keyword(s):  
Heat Transfer ◽  
Supersonic Flow ◽  
Blunt Body ◽  
Hydrogen Mixture
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