Abstract
A numerical method for solving inviscid steady-state two-dimensional flows is presented and extended to viscous flows. A system of quasi-one-dimensional governing equations applicable to both direct as well as inverse design problems for computing incompressible, subsonic and supersonic flows is derived. A pressure based flux split finite difference approximation is used along the streamlines. The method does not require any complicated grid generation technique. Applications are presented for both direct and inverse problems. The results are compared with exact solutions whenever available.
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