Program uses higher-order far field drag minimization. Computer program WDES WDEM preliminary aerodynamic design tool for one or two interacting, subsonic lifting surfaces. Subcritical wing design code employs higher-order far-field drag minimization technique. Linearized aerodynamic theory used. Program written in FORTRAN IV.
Interactive Graphics Analysis for Aircraft Design
NASA Tech Briefs ; 7 , 4
1983-10-01
Miscellaneous
No indication
English
Effects of interactive graphics on the aircraft design process
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