WINGDES2 computer program provides wing-design algorithm based on modified linear theory taking into account effects of attainable leading-edge thrust. Features improved numerical accuracy and additional capabilities. Provides analysis as well as design capability and applicable to both subsonic and supersonic flow. Replaces earlier wing-design code designated WINGDES (see LAR-13315). Written in FORTRAN V.
Wing-Design And -Analysis Code
NASA Tech Briefs ; 14 , 10
1990-10-01
Miscellaneous
No indication
English
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