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Span Load Distributions Resulting From Angle of Attack, Rolling, and Pitching for Tapered Sweptback Wings With Streamwise Tips. Supersonic Leading and Trailing Edges

John C. Martin, Isabella Jeffreys

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Key concepts: Angle of attack, Supersonic speed, Span (engineering), Trailing edge, Swept wing, Mechanics, Structural engineering, Materials science

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Span Load Distributions Resulting From Angle of Attack, Rolling, and Pitching for Tapered Sweptback Wings With Streamwise Tips. Supersonic Leading and Trailing Edges — Research Paper | ScholarLens