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The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. III : Effects of Trailing-edge Flaps

Bruce E Tinling, A. V. Karpen

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Key concepts: Airplane, Wing, Aerodynamics, Trailing edge, Leading edge, Aspect ratio (aeronautics), Aerospace engineering, Wing configuration

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The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. III : Effects of Trailing-edge Flaps — Research Paper | ScholarLens