A real gas laminar boundary-layer separation methodology has been developed to predict Space Shuttle Orbiter control surface effectiveness during atmospheric entry. The methodology is based on the Lees-Klineberg moment integral theory. A real gas laminar boundary-layer model, having a binary atomic diffusion of frozen gas composition, is assumed. A brief discussion of theory and sample results are presented herein. A set of boundary-layer profile parameters which are required for this theory is given in the full paper. (Jensen)
Real gas laminar boundary-layer separation prediction methodology
Methode der Vorhersage der Stroemungsabtrennung bei laminarer Grenzschichtstroemung
AIAA Journal ; 17 , 11 ; 1157-1158
1979
2 Seiten, 4 Bilder, 4 Quellen
Aufsatz (Zeitschrift)
Englisch
On laminar boundary-layer separation
AIAA | 1974
|Laminar boundary-layer separation in hypersonic flow.
AIAA | 1967
|