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The Dynamic Response Analysis of Launch Vehicle with ReducingPayload’s Fundamental Frequency
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School of Aeronautics,School of Aeronautics,School of Aeronautics,School of Aeronautics

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    Abstract:

    In this article we lead different fundamental frequency to the launch vehicle’s longitudinal model.By changing the frequency, vehicle’s dynamic response analysis is analyzed with finite element method and calculate the acceleration/element force response on payload with the changing of jet thrust . It discovers that the fundamental frequency affects the dynamic response of the launch vehicle;The effect is more patency on payload than other parts;The smaller frequency is,the bigger acceleration response of payload.

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GUO Feng, WAN Xiao-peng, ZHAO Mei-ying, SUN Ke. The Dynamic Response Analysis of Launch Vehicle with ReducingPayload’s Fundamental Frequency[J]. Advances in Aeronautical Science and Engineering,2013,4(4):438-442

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History
  • Received:October 17,2012
  • Revised:February 27,2013
  • Adopted:March 07,2013
  • Online: March 03,2014
  • Published: