Cyber 205 dense-mesh solutions to the Euler equations for flows around the M6 and Dillner wings
The dense-mesh solutions presented here have shown that the flowfield around a trapezoidal wing like the M6 can be represented with reasonable accuracy on a standard-size mesh of say 50,000 grid points. But if the wing is one of low aspect ratio, like the Dillner delta wing, a much denser grid is required to capture the rich structure of rotating flow interacting with shock waves.
KeywordsShock Wave Euler Equation Vortex Sheet Total Pressure Loss Delta Wing
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