WebMar 3, 2024 · These transonic flow conditions will cause the typical “lambda” shock along the upper surface of the lifting wing. Mesh Description. The computational domain is a large parallelepiped with the wing half-span mounted on one boundary in the x-z plane. The mesh consists of 582,752 tetrahedral elements and 108,396 nodes. http://www.ims.cuhk.edu.hk/publications/reports/2024-01.pdf
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