Publikationsdatum:
2011-08-16
Beschreibung:
The application of Rose's (1970) analytical method to the study of a shock wave interacting with a turbulent layer on a blunted compression surface is described. Only those details of the method that specifically apply to the case under consideration are discussed.
Schlagwort(e):
AERODYNAMICS
Materialart:
Journal of Spacecraft and Rockets; 9; Apr. 197
Format:
text