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Flutter analysis for control surface of launch vehicle with dynamic stiffness

Author(s):

Medium: journal article
Language(s): English
Published in: Computers & Structures, , n. 4, v. 60
Page(s): 593-599
DOI: 10.1016/0045-7949(95)00425-4
Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.1016/0045-7949(95)00425-4.
  • About this
    data sheet
  • Reference-ID
    10279402
  • Published on:
    05/01/2019
  • Last updated on:
    05/01/2019
 
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