测力试验结果表明，卷弧翼弹型存在自诱导滚转力矩。
The results on aerodynamic force demonstrated that the wrap around fin (WAF) configuration exhibits a self-induced rolling moment.
测力试验结果表明，卷弧翼弹型存在自诱导滚转力矩。
The results on aerodynamic force demonstrated that the wrap around fin (WAF) configuration exhibits a self-induced rolling moment.
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