Matrix-free aerostructural optimization of aircraft wings

In structural optimization subject to failure constraints, computing the gradients of a large number of functions with respect to a large number of design variables may not be computationally practical. Often, the number of constraints in these optimization problems is reduced using constraint aggre...

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Bibliographic Details
Published inStructural and multidisciplinary optimization Vol. 53; no. 3; pp. 589 - 603
Main Authors Lambe, Andrew B., Martins, Joaquim R. R. A.
Format Journal Article
LanguageEnglish
Published Berlin/Heidelberg Springer Berlin Heidelberg 01.03.2016
Springer Nature B.V
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