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Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration having a 60 degree delta wing and a high unswept horizontal tail

Robert F. Peck, Jesse L Mitchell

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Key concepts: Airplane, Aerospace engineering, Delta, Drag, Rocket (weapon), Degree (music), Lift-induced drag, Delta wing

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Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration having a 60 degree delta wing and a high unswept horizontal tail — Research Paper | ScholarLens