Effect of nose shape on hypersonic flow past slender blunt bodies at an angle of attack

1972 ◽  
Vol 4 (3) ◽  
pp. 140-143 ◽  
Author(s):  
B. A. Zemlyanskii ◽  
V. V. Lunev ◽  
K. M. Magomedov
Keyword(s):  
Hypersonic Flow ◽  
Angle Of Attack ◽  
Flow Past ◽  
Blunt Bodies ◽  
Nose Shape

Hypersonic flow-past of plane blunt bodies by a nonviscous radiating gas

1976 ◽  
Vol 16 (3) ◽  
pp. 365-370
Author(s):  
N. N. Pilyugin ◽  
G. A. Tirskii
Keyword(s):  
Hypersonic Flow ◽  
Flow Past ◽  
Blunt Bodies

Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection

1988 ◽  
Vol 22 (5) ◽  
pp. 737-742 ◽  
Author(s):  
V. A. Antonov ◽  
A. M. Grishin ◽  
F. M. Pakhomov
Keyword(s):  
Supersonic Flow ◽  
Angle Of Attack ◽  
Flow Past ◽  
Blunt Bodies

The Effects of Vibrational Relaxation on Hypersonic Flow Past Blunt Bodies

1997 ◽  
Vol 14 (4) ◽  
pp. 357-373 ◽  
Author(s):  
P. A. Blythe
Keyword(s):  
Hypersonic Flow ◽  
Vibrational Relaxation ◽  
Bluff Body ◽  
Flow Past ◽  
Equilibrium Parameter ◽  
Blunt Bodies ◽  
Relaxing Gas ◽  
Non Equilibrium

SummaryThe analysis of Freeman is extended to the hypersonic flow of an inviscid, vibrationally relaxing gas past a bluff body. Expressions for the shock shape, streamline shapes and stand-off distance are derived; these expressions have been evaluated for a sphere for various values of an appropriate non-equilibrium parameter Λ.

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