Vortex-lattice subsonic method determines mean camber surface for trimmed noncoplanar planforms with minimum vortex drag. Multiple surfaces can be designed together to yield trimmed configuration with minimum induced drag at some specified lift coefficient. Program is applicable to isolated wings, wing-canard configuration, tandem wing, and wing-winglet configuration.
Trimmed noncoplanar planforms with minimum vortex drag
NASA Tech Briefs ; 1 , 4
1977-03-01
Sonstige
Keine Angabe
Englisch
Minimum Trimmed Drag and Optimum c.g. Position
AIAA | 1978
|Crescent Wing Planforms Reduce Lift-Dependent Drag
NTRS | 1991
|Computing Trimmed, Mean-Camber Surfaces at Minimum Drag
Online Contents | 1995
Computing Trimmed, Mean-Camber Surfaces At Minimum Drag
NTRS | 1995
|