Lay-Up Optimization of Composite Stiffened Panels Using Linear Approximations in Lamination Space
By J. Herencia, Raphael T. Haftka, Paul M. Weaver, Michael I. Friswell. 2008
69 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/c8e5a4ef07aa39b4b6f2e6fb1dddce769376257c
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In Aerospace Engineering
In Civil and Structural Engineering
- Gabriel Delgado
- Osvaldo M. Querin
- Grégoire Allaire
- Dianzi Liu
- Krishnan Suresh
- Michael Y. Wang
- François Jouve
- Ole Sigmund
In Mechanics of Materials
Citations in the corpus
- Framework for the Buckling Optimization of Variable-Angle Tow Composite Plates (2015, unknown): “further optimized by adding the buckling load as a sensitivity-based constraint [43,44].”
- Bilevel Optimization of Blended Composite Wing Panels (2011, methodology): “In addition, a group of relationships between the in-plane and out-ofplane lamination parameters for the symmetric laminates are available (see [12–15,30,31]).”
- Stacking sequence and shape optimization of laminated composite plates via a level-set method (2016, methodology): “the penalty function approach [13, 66] and a rounding procedure using lamination parameters [32, 33, 67].”