CFD in Matlab
Hello 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
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