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CFD in MatlabHello Everyone ,
I wrote code to solve complete Navier stokes equation in Matlab for supersonic flow over flat plate . My doubt is Whether the Complete NS Equations predict the flow properties for hypersonic flows too ? . If so why do they have Viscous Shock Layer equations and Paralolized Navier Stokes Equations ? Also i wanted to know how to numerically discretize the Viscous shock layer equations for modelling Hypersonic flows in matlab . It would be of great help if someone share their knowledge Thanks :confused::confused::confused: |

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