Experimental Investigation of Three-Dimensional Flow Development by Pitching Low-Aspect-Ratio Wing (AIAA 2016-1066)
Aerospace sciences meeting
01.01.2016
19 pages
Aufsatz (Konferenz)
Englisch
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Control of Dynamic Stall Over a Pitching Finite-Aspect-Ratio Wing (AIAA 2017-4118)
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