Method predicts whole 2 and 3-dimensional hypersonic flow field, including shock wave curvatures and resulting vorticity; validity of method is checked by comparing predictions of theory with experiment for surface pressures and bow shock waves of bodies of revolution.
Generalized shock-expansion method and its application to bodies traveling at high supersonic air speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 4 ; p 231-238 + 248
1955
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1955
|Experiments on interaction of shock waves and cylindrical bodies at supersonic speeds
Engineering Index Backfile | 1952
|On calculation of flow about objects traveling at high supersonic speeds
Engineering Index Backfile | 1952
|Flow separation ahead blunt bodies at supersonic speeds
TIBKAT | 1951
|