Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamics
30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Leading-Edge Geometry on Delta Wing Unsteady Aerodynamics
Online Contents | 1993
|Nonlinear slender wing aerodynamics
AIAA | 1976
|Approximate Nonlinear Slender Wing Aerodynamics
AIAA | 1977
|