[PDF.13yv] Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A004 Airfoil Section - Transonic-Bump Method
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Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A004 Airfoil Section - Transonic-Bump Method
Myers; Boyd C II
[PDF.fr65] Aerodynamic Characteristics of a Wing with Unswept Quarter-Chord Line, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A004 Airfoil Section - Transonic-Bump Method
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