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Axial deformability of the composite lattice cylindrical shell under compressive loading: Application to a load-carrying spacecraft tubular body

Author(s):


Medium: journal article
Language(s): English
Published in: Composite Structures, , v. 146
Page(s): 201-206
DOI: 10.1016/j.compstruct.2016.03.021
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.compstruct.2016.03.021.
  • About this
    data sheet
  • Reference-ID
    10452895
  • Published on:
    23/10/2020
  • Last updated on:
    23/10/2020
 
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