Transonic flow calculations for rigid and flexible wings using a higher- order approximation method
This paper presents the transonic higher-order approximation method. This method is applicable to the transonic flow (in subsonic and low- supersonic free streams) over high and low aspect ratio rigid, flexible thin, and thick wings with or without control deflections. Typical computed results and their comparisons with wind tunnel test data are presented.
transonic higher-order approximation method
scientific article; zbMATH DE number 3954531