An inverse integral 3D compressible boundary layer method and coupling with transonic inviscid solution (Q1197325)

(From the authors' summary.) ``A new velocity profile, which has a simple expression and agrees well with experimental data in a wide range, has been proposed in this paper. Based on this profile, the governing equations of the 3D compressible inverse boundary layer method have been deduced. The steady transonic viscous flow around a 3D wing has been calculated as follows: the inviscid flow is calculated by using non- isentropic full potential equation; the viscous flow is calculated by using present boundary layer method; the viscous and inviscid solutions are coupled by using semi-inverse method. Numerical results agree well with the experimental data''.