Improved program based on more-accurate mathematical mode. WDAG2 calculates supersonic zero-lift wave drag of complex aircraft configurations. Incorporates extended capabilities for geometric input to enable use of more-accurate mathematical model. Engineer defines aircraft components as fusiform or non-fusiform by use of traditional parallel contours. Written in FORTRAN IV.
Calculating Wave Drag on an Aircraft
NASA Tech Briefs ; 11 , 9
1987-10-01
Sonstige
Keine Angabe
Englisch