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I have a 76/40 degree double delta wing. I want to find the bevel angle for the leading edge of the wing configuration. The root chord of the wing is 191 mm and wing span is 195 mm. Is there any...
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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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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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