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弹性飞行器对大气紊流的动力响应计算 被引量:2

CALCULATION OF DYNAMIC RESPONSE OF ELASTIC VEHICIES TO ATMOSPHERIC TWRBULENCE
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摘要 本文采用功率谱密度技术,分别从频域模型和时域状态空间模型给出了弹性飞行器对大气紊流动力响应计算方法,并通过实例计算,说明大气紊流对弹性飞行器的影响. In this paper, the calculation of dynamic response of elastic vehicles to atmospheric twrbulence based on power spectral density technique is studied. Two calculating methods are given, one of which is based on frequency domain model of elastic vehicle and the other is based on time domain state-(?)pace model. An example shows the effect of atmospheric turbalence on elastic vehicles.
机构地区 西北工业大学
出处 《飞行力学》 CSCD 北大核心 1992年第2期53-59,共7页 Flight Dynamics
关键词 弹性飞行器 大气紊流 动力响应 Elastic vehicle Atmospheric turbulence Power spectral density technique Dynamic response
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同被引文献17

  • 1杨智春,夏巍,孙浩.高速飞行器壁板颤振的分析模型和分析方法[J].应用力学学报,2006,23(4):537-542. 被引量:29
  • 2吴志刚,杨超.弹性导弹的连续与离散阵风响应[J].北京航空航天大学学报,2007,33(2):136-140. 被引量:16
  • 3邱传仁 周文伯 严震.飞机对大气紊流的动态响应.上海交通大学学报,1986,20(6):76-84.
  • 4Kim T U, Hwang I H. Reliability analysis of composite wing subjected to gust loads [ J ]. Composite structures, 2004,66: 527 - 531.
  • 5Chen R R, Blosser M L. Metallic thernal projection system panel flutter study [ J ]. AIAA Paper 02 - 0501, 2002.
  • 6肖业伦,金长江.大气扰动中的飞行原理[M].国防工业出版社,1993,48-72.
  • 7Yang Y R. KBM method of analyzing limit cycle flutter of a wing with an external store and comparison with a wind-tunnel test [ J ]. Journal of Sound and Vibration, 1995, 187 (2) :271 - 280.
  • 8Yang Z C, Zhao L C. Analysis of limit cycle flutter of an airfoil in incompressible flow [ J ]. Journal of Sound and Vibration, 1988, 123(1):1 -13.
  • 9邱传仁 周文伯 严震.飞机对连续型大气紊流的动态响应.上海交通大学学报,1986,20(6):76-84.
  • 10Kim T-U, Hwang I H. Reliability analysis of composite wing subjected to gust loads [J]. Composite Structures, 2004, 66: 527--531.

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