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A refined optimality criterion technique applied to aircraft wing structural design

Author(s):

Medium: journal article
Language(s): English
Published in: Computers & Structures, , n. 2, v. 33
Page(s): 427-434
DOI: 10.1016/0045-7949(89)90014-x
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(89)90014-x.
  • About this
    data sheet
  • Reference-ID
    10275952
  • Published on:
    05/01/2019
  • Last updated on:
    05/01/2019
 
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