A numerical method is presented for predicting the aerodynamic characteristics of elastic aircraft under quasi-static approximation.
本文介绍一种准静弹性飞机气动特性的数值计算方法。
A numerical method is presented for predicting the aerodynamic characteristics of elastic aircraft under quasi-static approximation.
本文介绍一种准静弹性飞机气动特性的数值计算方法。
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