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Application of a simple hole damage stress analysis method to composite airframes: Case studies

Author(s):
Medium: journal article
Language(s): English
Published in: Composite Structures, , n. 3, v. 27
Page(s): 253-259
DOI: 10.1016/0263-8223(94)90086-8
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: 10.1016/0263-8223(94)90086-8.
  • About this
    data sheet
  • Reference-ID
    10459590
  • Published on:
    25/10/2020
  • Last updated on:
    25/10/2020
 
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