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Hinge-moment and control-effectiveness characteristics of an outboard flap with an overhang nose balance on a tapered 35 degree sweptback wing of aspect ratio 4 : transonic-bump method

Robert Thompson, William C Moseley

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Abstract

Report presenting an investigation in the high-speed tunnel to determine the hinge-moment and control-effectiveness characteristics of a tapered, 35 degree sweptback, semispan wing equipped with an outboard 43-percent-span flap. Results regarding the lift, rolling-moment, and pitching-moment characteristics are provided.

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Report presenting an investigation in the high-speed tunnel to determine the hinge-moment and control-effectiveness characteristics of a tapered, 35 degree sweptback, semispan wing equipped with an outboard 43-percent-span flap. Results regarding the lift, rolling-moment, and pitching-moment characteristics are provided.

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Available abstract

Report presenting an investigation in the high-speed tunnel to determine the hinge-moment and control-effectiveness characteristics of a tapered, 35 degree sweptback, semispan wing equipped with an outboard 43-percent-span flap. Results regarding the lift, rolling-moment, and pitching-moment characteristics are provided.

Key concepts: Wing, Hinge, Moment (physics), Structural engineering, Balance (ability), Engineering, Physical medicine and rehabilitation, Medicine

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Hinge-moment and control-effectiveness characteristics of an outboard flap with an overhang nose balance on a tapered 35 degree sweptback wing of aspect ratio 4 : transonic-bump method — Research Paper | ScholarLens