Pressure distribution on thin nonlifting airfoils in steady two dimensional flow with freestream Mach number at or near unity
Flow with M/infinity/equals 1 past thin airfoils
1970-10-01
Sonstige
Keine Angabe
Englisch
Flow with M/infinity/equals 1 past thin airfoils
AIAA | 1970
|Wedge and cone theory for m infinity equals infinity.
AIAA | 1965
|Wedge and cone theory for m infinity equals infinity.
NTRS | 1965
|AIAA | 1963
|Comments on Flow with Moo = 1 Past Thin Airfoils
AIAA | 1971
|