Predicted drag values for a given airfoil(RAE2822 airfoil)were compared and discussed using the surface integration and wake integration methods under both subsonic and supercritical flow conditions.

在亚跨声速时分别采用了表面积分和尾迹积分求得给定翼型RAE2822的阻力。

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Predicted drag values for a given airfoil(RAE2822 airfoil)were compared and discussed using the surface integration and wake integration methods under both subsonic and supercritical flow conditions.

在亚跨声速时分别采用了表面积分和尾迹积分求得给定翼型RAE2822的阻力。

youdao