Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

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A note on subsonic edges in unsteady supersonic flow


Author: John W. Miles
Journal: Quart. Appl. Math. 11 (1953), 363-367
MSC: Primary 76.1X
DOI: https://doi.org/10.1090/qam/57122
MathSciNet review: 57122
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Abstract: The pressure distribution due to the unsteady motion of a wing having a supersonic leading edge and a subsonic trailing edge is determined by applying a Lorentz transformation to the corresponding result for a rectangular wing. This result, valid as it stands for a subsonic leading edge, is then modified by the addition of an eigensolution in order to satisfy the Kutta condition.


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DOI: https://doi.org/10.1090/qam/57122
Article copyright: © Copyright 1953 American Mathematical Society


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