Computational Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing (AIAA 2018-0357)
Aerospace sciences meeting ; 2018 ; Kissimmee, FL
2018-01-01
23 pages
Aufsatz (Konferenz)
Englisch
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Control of Dynamic Stall Over a Pitching Finite-Aspect-Ratio Wing (AIAA 2017-4118)
British Library Conference Proceedings | 2017
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