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Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions

Kenneth P Spreemann

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Key concepts: Fuselage, Chord (peer-to-peer), Wing, Aerodynamics, Leading edge, RADIUS, Enhanced Data Rates for GSM Evolution, Aerospace engineering

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Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions — Research Paper | ScholarLens