Computational Results for 2-D and 3-D Ramp Flows with an Upwind Navier-Stokes Solver
An implicit, finite-difference, upwind, full Navier-Stokes solver has been applied to supersonic/hypersonic flows over two-dimensional ramps and three-dimensional obstacle (Problem sets 3 and 4). Some of the computed numerical results are presented here.
KeywordsHeat Transfer Coefficient Skin Friction Fine Grid Skin Friction Coefficient Sweep Line
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