A refined optimality criterion technique applied to aircraft wing structural design

DOI10.1016/0045-7949(89)90014-XzbMath0698.73070OpenAlexW2009297581MaRDI QIDQ3476414

Chien-Chang Lin, Ine-Wei Liu

Publication date: 1989

Published in: Computers & Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7949(89)90014-x

zbMATH Keywords

finite element methodsensitivity analysisoptimal designKuhn-Tucker conditionsFORTRAN-77fully stressed designAutomatic Resizing System 4modular computer program `ARS 4'refined optimality criterion methodwing structures subjected to size, stress, displacement, and buckling constraints

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Optimization problems in solid mechanics (74P99) Software, source code, etc. for problems pertaining to mechanics of deformable solids (74-04)

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