A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
1957
41 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aerodynamic characteristics , Conical camber , Tail , Triangular wing , Wing body , Body , Camber , Characteristics , Coefficient , Conical , Drag , Lift , Subsonic , Supersonic , Transonic , Triangle , Tunnel , Wind , Wing
Slender Delta Wing with Conical Camber
AIAA | 1974
|Airplane wing leading edge variable camber flap
NTRS | 1980
|