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Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3

Allen B Henning

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Key concepts: Mach number, Longitudinal static stability, Aerospace engineering, Lift-to-drag ratio, Lift (data mining), Drag, Lift-induced drag, Aeronautics

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Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3 — Research Paper | ScholarLens