Through the numerical calculations of ONERA M6 wing. LANN wing and a rectangular wing, the correctness and validity of the numerical simulation of Euler equation using the approximate boundary conditions on 3-D flow are validated.

 
  • 通過(guò)對M6機翼、LANN機翼和平直矩形機翼的數值計算,驗證了采用近似邊界條件的Euler方程在三維流動(dòng)數值模擬中的正確性和有效性。
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