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Uncertainty-based loads analysis for spacecraft: Finite element model validation and dynamic responses

Author(s):
Medium: journal article
Language(s): English
Published in: Computers & Structures, , n. 14, v. 83
Page(s): 1103-1112
DOI: 10.1016/j.compstruc.2004.11.019
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.2004.11.019.
  • About this
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  • Reference-ID
    10281547
  • Published on:
    05/01/2019
  • Last updated on:
    05/01/2019
 
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