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Numerical solution of supersonic flow in compression corner

version 1.0.0 (9.23 KB) by Ivan
Solves the Euler equations numerically to compute the supersonic flow across a compression corner.

8 Downloads

Updated 10 Jun 2020

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This code solves the Euler equations numerically to compute the supersonic flow across a compression corner. The associated oblique shock is captured by the numerical solution and is compared against the analytical solution provided by the oblique shock relations.

The numerical technique employed is very basic and follows the methodology described in Chapter 7 of the book "Computational fluid dynamics: the basics with applications" (1995) from J.D.Anderson.

This is a good academic test case for anyone interested in learning CFD and compressible flow.

Cite As

Ivan (2020). Numerical solution of supersonic flow in compression corner (https://www.mathworks.com/matlabcentral/fileexchange/76802-numerical-solution-of-supersonic-flow-in-compression-corner), MATLAB Central File Exchange. Retrieved .

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MATLAB Release Compatibility
Created with R2020a
Compatible with any release
Platform Compatibility
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