The dynamic response of an aircraft windshield to bird-impact loading was simulated by the proposed analysis model.

 
  • 對某飛機風(fēng)擋進(jìn)行了動(dòng)響應分析,計算了風(fēng)擋中軸線(xiàn)上四點(diǎn)位移時(shí)間曲線(xiàn);
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