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Static lateral stability characteristics of a 1/16 scale model of the Douglas D-558-II research airplane at Mach numbers of 1.61 and 2.01

Frederick C. Grant, Ross B Robinson

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Key concepts: Airplane, Mach number, Stability (learning theory), Scale (ratio), Aeronautics, Computer science, Aerospace engineering, Engineering

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Static lateral stability characteristics of a 1/16 scale model of the Douglas D-558-II research airplane at Mach numbers of 1.61 and 2.01 — Research Paper | ScholarLens