The aerodynamic characteristics of slender delta wings for subsonic commercial aircraft applications are discussed. The flow distribution on the wing for various airspeed conditions is described. The characteristics of conventional wings are compared with those of the slender delta wing. Graphs of the performance of the slender delta wing for various conditions of ground effect, angle of attack, glide conditions, and aerodynamic stall are included. (Author)
Slender delta Wings for Future Subsonic Commercial Aircraft
1973
28 pages
Report
No indication
English
Subsonic wing rock of slender delta wings
AIAA | 1985
|Subsonic wing rock of slender delta wings
AIAA | 1985
|Subsonic vortex-flow design study for slender wings
AIAA | 1978
|