Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringe (AIAA 2015-1707)
Aerospace sciences meeting
01.01.2015
13 pages
Aufsatz (Konferenz)
Englisch
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Wake Vortex Field of an Airfoil Equipped with an Active Finite Gurney Flap (AIAA 2015-1271)
British Library Conference Proceedings | 2015
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