Direct Numerical Simulation Of Hypersonic Boundary-Layer Transition Over A Blunt Cone
作者： Xinliang Li , Dexun Fu , Yanwen Ma
DOI: 10.2514/1.37305
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摘要: … To test our code, we compare our result with the results of Zhong and Ma [7]. Our steady numerical simulation is carried out on a mesh with 1600 (streamwise) 160 (wall normal) 8 (circumference) grid points. Because the attack of angle is zero, the steady flow is two-dimensional (axisymmetrical), and the mesh number in circumference does not affect the numerical accuracy. … Those two figures show very good agreement between our numerical results and the results of Zhong and Ma [7]. Unlike wall pressure, the numerical result of wall temperature is very sensitive to …
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