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Experimental and predicted longitudinal response characteristics of a large flexible 35-degree swept-wing airplane at an altitude of 35,000 feet

H. A. Cole, Stuart C. Brown, E. C. Holleman

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Key concepts: Airplane, Wing, Degree (music), Altitude (triangle), Wing loading, Aeronautics, Aerospace engineering, Engineering

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Experimental and predicted longitudinal response characteristics of a large flexible 35-degree swept-wing airplane at an altitude of 35,000 feet — Research Paper | ScholarLens