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I need to simulate a flat plate in a hypersonic flow of Mach 8 to visualize the heat profile over the flat plate. Currently i am using a velocity inlet, outlet, and symmetry over the sides of the...
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I need someone to explain the last term in the equation, and how do I calculate them for a mach 8 flow over a cylinder?
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Technically speaking the total temperature should not change across a shock. But when I tried Simulating a Hypersonic flow across a conical body (0 AOA), you can see that the temperature across...
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I need to simulate a flow in a hypersonic wind tunnel, using CFD(Fluent). But I'm having problems setting up the boundary conditions to simulate the flow. People who can help me please do...
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