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                                       Details for article 4 of 139 found articles
 
 
  Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method
 
 
Title: Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method
Author: Abdullah, Nur Azam
Curiel-Sosa, Jose Luis
Akbar, Mahesa
Appeared in: Composite structures
Paging: Volume 202 (2018) nr. C pages 151-161
Year: 2018
Contents:
Publisher: Elsevier Ltd
Source file: Elektronische Wetenschappelijke Tijdschriften
 
 

                             Details for article 4 of 139 found articles
 
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