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A multidisciplinary design optimization approach for high temperature aircraft engine components

Author(s):


Medium: journal article
Language(s): English
Published in: Structural Optimization, , n. 2-3, v. 18
Page(s): 134
DOI: 10.1007/s001580050114
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: 10.1007/s001580050114.
  • About this
    data sheet
  • Reference-ID
    10344705
  • Published on:
    14/08/2019
  • Last updated on:
    14/08/2019
 
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