High-Fidelity Aerostructural Optimization with a Geometrically Nonlinear Flutter Constraint
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DOI: 10.2514/1.j062127
Abstract: When designing aircraft, avoiding dynamic aeroelastic instabilities such as flutter is a key requirement. One way to meet this requirement is to use a multidisciplinary design optimization subject to a flutter constraint. Flutter-constrained design optimizations… read more here.
Keywords: geometrically nonlinear; nonlinear flutter; flutter constraint; flutter ... See more keywords