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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Published in | Structural and multidisciplinary optimization Vol. 53; no. 3; pp. 589 - 603 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Berlin/Heidelberg
Springer Berlin Heidelberg
01.03.2016
Springer Nature B.V |
Subjects | |
Online Access | Get full text |
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