Sign Up to like & get
recommendations!
0
Published in 2019 at "Composite Structures"
DOI: 10.1016/j.compstruct.2018.10.062
Abstract: Composite materials are finding increasing application, for example in commercial aircraft. Traditionally fiber angles are restricted to 0°,±45° and 90°. The current work exploits the possibility of using multiple ’non-conventional’ laminates where either fiber steering…
read more here.
Keywords:
buckling load;
non conventional;
conventional laminates;
optimal design ... See more keywords