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CFD solution of quasi-1D nozzle flows using finite difference approach

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quasi-1D Nozzle Flows

Contains quasi-one-dimensional flow through a convergent-divergent nozzle with and without shock capturing. In quasi_1D_without_shock.m, the finite difference expression is set up using MacCormack's explicit technique for the numerical solution of governing equations in non-conservation form; however, for the shock-capturing method, which is used in quasi_1D_with_shock_capturing.m, the conservation form of governing equations is employed. This problem is taken from chapter 7 of the textbook "Computational Fluid Dynamics: The Basics with Applications" by JD Anderson. I have also attached the document to make it easy to follow the formulations and codes. These codes are for educational purposes.

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CFD solution of quasi-1D nozzle flows using finite difference approach

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