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Multiobjective optimization of vane-type vortex generators (VGs) on swept wings are conducted to provide designs that are suitable for both cruise and critical conditions. The optimization is divided into two phases: the VG arrangement is optimized on a three-dimensional transonic aircraft after the VG shape is optimized on a swept infinite wing.

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This page is a summary of: Multipoint Design Optimization of Vortex Generators on Transonic Swept Wings, Journal of Aircraft, March 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035148.
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