Scramjet intake

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The inflow conditions are * Mach =5.0 * ρ=1.0 * u=1.0 * v=0.0 ==Geometry== [[Image:Vtc_scramjet_geometry.png | Scramjet geometry]] ==Density contours== [[Image:Vtc_scramjet_density.png | Scramjet - Density contours]] ==References== *{{reference-paper | author=Kumar, A. | year=1981 | title=Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations | rest=Technical Paper 1940, NASA}}

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