Effect of large blowing rates on the compressible boundary layer flow at the stagnation point of a rotating sphere
The effect of a large surface blowing (injection) rate on the steady laminar compressible boundary-layer flow at the forward stagnation point of a rotating sphere has been studied. The resulting coupled nonlinear ordinary differential equations have been solved using two methods, namely, the method of matched asymptotic expansion and the implicit finite difference scheme in combination with the quasilinearization technique.
scientific article; zbMATH DE number 1019275