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Influence of optimized leading-edge deflection and geometric anhedral on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration. [langley 7 by 10 foot tunnel]

P. L. Coe, J. K. Huffman

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Key concepts: Deflection (physics), Wing, Aerodynamics, Leading edge, Aspect ratio (aeronautics), Engineering, Aerospace engineering, Physics

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Influence of optimized leading-edge deflection and geometric anhedral on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration. [langley 7 by 10 foot tunnel] — Research Paper | ScholarLens