A computational transonic design procedure for three-dimensional wings in which shapes are determined supporting prescribed pressure distributions, is presented. The method uses an existing three-dimensional modified small disturbance theory analysis code to include the design procedure. A consistent analysis-design differencing procedure at the wing slit is implemented. Design results are presented for aft and forward swept wings in isolation as well as in the presence of a fuselage. Performance of the designed wing at off-design Mach number and in the presence of solid and free jet wind tunnel walls is also reported. (DePo)
Computational transonic design procedure for three-dimensional wings and wing-body combinations
Rechnergestuetzte Konstruktion dreidimensionaler Fluegel und von Fluegel-Koerperkombinationen fuer den transsonischen Bereich
AIAA-Papers ; 1-14
1979
14 Seiten, 11 Bilder, 17 Quellen
Conference paper
English