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The static longitudinal characteristics of a twisted and cambered 45 degree sweptback wing at Mach numbers up to 0.96

Robert I Sammonds, R. M. Reynolds

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Abstract

Report presenting a 45 degree sweptback wing of aspect ratio 3, with twist and a distributed type of camber, tested in combination with a body of fineness ratio 12.5 to determine the lift, drag, and pitching-moment characteristics.

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Report presenting a 45 degree sweptback wing of aspect ratio 3, with twist and a distributed type of camber, tested in combination with a body of fineness ratio 12.5 to determine the lift, drag, and pitching-moment characteristics.

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Available abstract

Report presenting a 45 degree sweptback wing of aspect ratio 3, with twist and a distributed type of camber, tested in combination with a body of fineness ratio 12.5 to determine the lift, drag, and pitching-moment characteristics.

Key concepts: Wing, Camber (aerodynamics), Drag, Degree (music), Lift (data mining), Lift-induced drag, Structural engineering, Fineness

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The static longitudinal characteristics of a twisted and cambered 45 degree sweptback wing at Mach numbers up to 0.96 — Research Paper | ScholarLens