A streamline curvature method for design of supercritical and subcritical airfoils
暂无分享,去创建一个
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described. The method is based on the streamline curvature velocity equation. Several examples illustrating this method are presented and discussed.
[1] T. Strand,et al. Exact Method of Designing Airfoils With Given Velocity Distribution in Incompressible Flow , 1973 .
[2] P. R. Garabedian,et al. Analysis of transonic airfoils. , 1971 .
[3] G. Y. Nieuwland. Theoretical design of shock free, transonic flow around aerofoil sections , 1966 .
[4] Richard M. James,et al. A General Class of Exact Airfoil Solutions , 1972 .