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Small-scale transonic investigation of the effects of full-span and partial-leading-edge flaps on the aerodynamic characteristics of a 50 degree 38 foot sweptback wing of aspect ratio 2.98

Kenneth P Spreeman, W. J. Alford

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Key concepts: Wing, Transonic, Aerodynamics, Leading edge, Degree (music), Span (engineering), Structural engineering, Scale (ratio)

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Small-scale transonic investigation of the effects of full-span and partial-leading-edge flaps on the aerodynamic characteristics of a 50 degree 38 foot sweptback wing of aspect ratio 2.98 — Research Paper | ScholarLens