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本文给出了亚、超音速弧翼的滚转及偏航阻尼力矩特性,并从理论上证明了零攻角时有厚度弧翼在亚、超音速绕流时正、反向滚转的必然性。
In this paper, the roll and yaw damping torque characteristics of sub-supersonic arc are given, and the necessity of roll-forward and reverse roll of thickness arc at the time of sub-AOA is proved theoretically .