Analytical procedures used to evaluate the application of suction boundary-layer control (BLC) to subsonic V/STOL inlets are presented. These procedures have been used to analytically predict the optimum (minimum suction power required) location and extent for a suction slot of two different surface resistances within a subsonic V/STOL inlet. Results of this analytical study are presented.
Analytical study of suction boundary layer control for subsonic V/STOL inlets
01.06.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
Zero-length inlets for subsonic V/STOL aircraft
AIAA | 1983
|Zero-length inlets for subsonic V/STOL aircraft
NTRS | 1981
|Zero-length inlets for subsonic V/STOL aircraft
AIAA | 1981
|