An Unsteady Aerodynamic Model based on the Leading-Edge Stagnation Point (AIAA 2015-3309)
Applied aerodynamics ; 2015 ; Dallas, TX
2015-01-01
21 pages
Conference paper
English
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Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point
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|Unsteady Aerodynamic Model Based on the Leading-Edge Stagnation Point
Online Contents | 2016
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