Analytical solutions for hypersonic flow past slender power-law bodies at small angle of attack

AIAA Journal ◽  
1992 ◽  
Vol 30 (11) ◽  
pp. 2683-2693 ◽  
Author(s):  
A. Merlen ◽  
D. Andriamanalina
Keyword(s):  
Hypersonic Flow ◽  
Power Law ◽  
Analytical Solutions ◽  
Small Angle ◽  
Angle Of Attack ◽  
Flow Past

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

On hypersonic flow past conical segment bodies at large angle of attack

1973 ◽  
Vol 5 (3) ◽  
pp. 382-387
Author(s):  
B. A. Zemlyanskii
Keyword(s):  
Hypersonic Flow ◽  
Angle Of Attack ◽  
Large Angle ◽  
Flow Past

scholarly journals Mixed convection flow past a horizontal plate

2005 ◽  
Vol 32 (1) ◽  
pp. 1-19 ◽  
Author(s):  
Lj. Savic ◽  
H. Steinrück
Keyword(s):  
Mixed Convection ◽  
Small Angle ◽  
Potential Flow ◽  
Lift Coefficient ◽  
Angle Of Attack ◽  
Large Reynolds Number ◽  
Convection Flow ◽  
Horizontal Plate ◽  
Mixed Convection Flow ◽  
Flow Past

The mixed convection flow past a horizontal plate being aligned through a small angle of attack to a uniform free stream will be considered in the limit of large Reynolds number and small Richardson number. Even a small angle of inclination of the wake is sufficient for the buoyancy force to accelerate the flow in the wake which causes a velocity overshoot in the wake. Moreover a hydrostatic pressure difference across the wake induces a correction to the potential flow which influences the inclination of the wake. Thus the wake and the correction of the potential flow have to be determined simultaneously. However, it turns out that solutions exist only if the angle of attack is sufficiently large. Solutions are computed numerically and the influence of the buoyancy on the lift coefficient is determined.

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