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EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03

F E West, George Liner, Gladys S. Martz

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Key concepts: Fuselage, Chord (peer-to-peer), Wing, Mach number, Aerodynamics, Leading edge, Structural engineering, Trailing edge

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EFFECT OF LEADING-EDGE CHORD-EXTENSIONS ON THE AERODYNAMIC CHARACTERISTICS OF A 45 SWEPTBACK WING-FUSELAGE COMBINATION AT MACH NUMBERS OF 0.40 TO 1.03 — Research Paper | ScholarLens