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Comparison of large scale flight measurements of zero lift drag at Mach numbers from 0.9 to 1.7 of two wing-body combinations having similar 60 degree triangular wings with NACA 65A003 sections

Eugene D Schult

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Key concepts: Vortex lift, Wing, Mach number, Lift (data mining), Degree (music), Lift-to-drag ratio, Drag, Zero (linguistics)

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Comparison of large scale flight measurements of zero lift drag at Mach numbers from 0.9 to 1.7 of two wing-body combinations having similar 60 degree triangular wings with NACA 65A003 sections — Research Paper | ScholarLens