scholarly journals Fore-Body Drag Reduction of a Blunt Body in Compressible Thrbulent Boundary Layer.

2002 ◽  
Vol 50 (586) ◽  
pp. 474-476
Author(s):  
Takafumi Yamawaki ◽  
Hideaki Ogawa ◽  
Takeo Okunuki ◽  
Hisao Koyama ◽  
Hiroshi Itoh ◽  
...  
AIAA Journal ◽  
2002 ◽  
Vol 40 ◽  
pp. 1178-1186 ◽  
Author(s):  
J. S. Shang

2010 ◽  
Vol 114 (1152) ◽  
pp. 113-119 ◽  
Author(s):  
G. d’Humières ◽  
J. L. Stollery

AbstractFitting a spike on a blunt body provides a drag reduction at supersonic and hypersonic speeds. In this study, the laminar flow over a spiked, conical body terminated by a spherical cap, inspired by the Apollo re-entry capsule design, was investigated using a hypersonic wind tunnel. Schlieren pictures revealed the absence of flow unsteadiness for the range of spike lengths tested, and force measurements showed a maximum reduction of 77% of the unspiked body drag.A simple theoretical model based on the pressure drag generated by a solid cone showed good agreement with the experimental data. The measured shock stand-off distance agreed well with predictions.


AIAA Journal ◽  
2002 ◽  
Vol 40 (6) ◽  
pp. 1178-1186 ◽  
Author(s):  
J. S. Shang

AIAA Journal ◽  
1999 ◽  
Vol 37 ◽  
pp. 460-467 ◽  
Author(s):  
David Riggins ◽  
H. F. Nelson ◽  
Eric Johnson

2003 ◽  
Author(s):  
Paul Dimotakis ◽  
Patrick Diamond ◽  
Freeman Dyson ◽  
David Hammer ◽  
Jonathan Katz

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