Effect of Slenderness Ratio on Free-to-Roll Wing Aerodynamics
Journal of aircraft ; 48 , 3 ; 1112-1116
2011
Aufsatz (Zeitschrift)
Englisch
Leading-Edge Vortex Breakdown for Wing Planforms with the Same Slenderness Ratio
Online Contents | 1994
|Aerodynamics of Free-to-Roll Low Aspect Ratio Wings
AIAA | 2009
|