An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point (AIAA 2015-3309)
Applied aerodynamics ; 2015 ; Dallas, TX
01.01.2015
21 pages
Aufsatz (Konferenz)
Englisch
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Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point
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Online Contents | 2016
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