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Structure of the Flow Associated with a Two-Dimensional Supersonic Intake
Published online by Cambridge University Press: 07 June 2016
Summary
The intake is conceived as a device that generates a shock system and a subsonic patch within a supersonic field. The object of the paper is to obtain a qualitative description of this flow structure. The analytical procedure is a simple but fairly powerful mapping technique. Several examples are discussed and these show how the flow on the intake alters under the influence of gradually changing boundary conditions.
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- Copyright © Royal Aeronautical Society. 1965
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