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A dynamic stiffness element for free vibration analysis of composite beams and its application to aircraft wings

Author(s):


Medium: journal article
Language(s): English
Published in: Computers & Structures, , n. 6, v. 86
Page(s): 573-579
DOI: 10.1016/j.compstruc.2007.04.027
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/j.compstruc.2007.04.027.
  • About this
    data sheet
  • Reference-ID
    10274466
  • Published on:
    05/01/2019
  • Last updated on:
    05/01/2019
 
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