flutter calculation

基本解释

The nonlinear flutter calculation demonstrates the validity of the presented method.
機翼的非線性顫振計算表明了方法的有傚性。
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In this paper a stiffness simulation calculation method of low speed flutter models of an aeroplane is studied.
本文探討了飛機低速顫振模型剛度模擬計算的一種方法。
The unsteady aerodynamic results of the transonic wing are presented, and flutter calculation is made. The comparison with TDLM shows that the agreement is very good.
對跨聲速飛機機翼作了跨聲速非定常氣動力計算，對跨聲速民航機機翼的顫振模型作了顫振計算，與TDLM的比較表明，兩者結果有較好的一致性。