Abstract
AbstractA finite difference scheme is presented for the solution of the two‐dimensional equations of steady, supersonic, isentropic flow. The scheme incorporates numerical characteristic decomposition, is shock‐capturing by design and incorporates space marching as a result of the assumption that the flow is wholly supersonic in at least one space dimension. Results are shown for problems involving oblique hydraulic jumps and reflection from a wall.
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More From: International Journal for Numerical Methods in Fluids
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