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.

• 通过对M6机翼、LANN机翼和平直矩形机翼的数值计算,验证了采用近似边界条件的Euler方程在三维流动数值模拟中的正确性和有效性。