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Maximum lift-drag-ratio characteristics of rectangular and delta wings at mach 6.9

J. A. Penland

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Key concepts: Vortex lift, Drag, Lift-to-drag ratio, Lift (data mining), Lift-induced drag, Delta wing, Mach number, Drag coefficient

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Maximum lift-drag-ratio characteristics of rectangular and delta wings at mach 6.9 — Research Paper | ScholarLens