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中文摘要：
使用灵活结构的自然颤动的形式的特征设计震荡的翅膀飞机被建议。有关灵活结构的震荡的翅膀的一系列方程被导出。为空气动力学的力量的运动方程结合了有弹性的运动被建立，并且相关公式被导出。在那个公式的不稳定的空气动力学的被修订。设计原则，设计过程和如此的震荡的翅膀的申请的范围分析方法被详细描述。一个灵活结构的震荡翅膀模型被建立，并且相关时间反应分析和频率反应分析被进行。分析结果显示那采用新型的开车方法因为震荡的翅膀没有拍翅问题并且将能生产推进的力量。而且，它将为产生一样的电梯比固定翅膀消费少得多力量。
英文摘要：
Making use of modal characteristics of the natural vibration of flexible structure to design the oscillating wing aircraft is proposed. A series of equations concerning the oscillating wing of flexible structures are derived. The kinetic equation for aerodynamic force coupled with elastic movement is set up, and relevant formulae are derived. The unsteady aerodynamic one in that formulae is revised. The design principle, design process and range of application of such oscillating wing analytical method are elaborated. A flexible structural oscillating wing model is set up, and relevant time response analysis and frequency response analysis are conducted. The analytical results indicate that adopting the new-type driving way for the oscillating wing will not have flutter problems and will be able to produce propulsive force. Furthermore, it will consume much less power than the fixed wing for generating the same lift.
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