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Theory of an Accelerated Slender Supersonic Aerofoil
Published online by Cambridge University Press: 07 June 2016
Summary
The problem of a uniformly accelerated slender supersonic aerofoil is solved in this paper by a perturbation method for the cases when the acceleration is small. Full account is taken of the effect of the acceleration on the form of the shock line.
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- Research Article
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- Copyright © Royal Aeronautical Society. 1954