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Optimum design of composite wing structures by a refined optimality criterion

  • Published:1991-01 Issue:1 Volume:17 Page:51-65
  • ISSN:0263-8223
  • Container-title:Composite Structures
  • language:en
  • Short-container-title:Composite Structures

Author:

Liu Ine-Wei,Lin Chien-Chang

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference12 articles.

1. Computer program (OPTCOMP) for optimization of composite structures for minimum weight design;Khot;AFFDL-TR-76-149,1977

2. OPTSTAT — A computer program for optimal design of structures subjected to static loads;Venkayya;AFFDL-TR-79-67,1979

3. A multilevel approach for minimum weight structural design including local and system buckling constraints;Schmit;AIAA Paper 77-373,1977

4. Preliminary design of composite wings for buckling, strength, and displacement constraints;Starnes;Journal of Aircraft,1979

5. Optimal design based on optimality criterion for frame structures including buckling constraints;Lin;Computers & Structures,1989

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1. Flutter characteristics of axially functional graded composite wing system;ADV AIRCR SPACECR SC;2020

2. Optimum Design of Composite Structures: A Literature Survey (1969–2009);Journal of Reinforced Plastics and Composites;2016-10-01

3. Structural Reliability Analysis of Composite Wing Subjected to Gust Loads;Proceedings of the International Symposium on Engineering under Uncertainty: Safety Assessment and Management (ISEUSAM - 2012);2012-12-06

4. Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-10-21

5. Stacking sequence design of a composite wing under a random gust using a genetic algorithm;Computers & Structures;2007-05
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