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- W1510230107 abstract "Summary An experimental study has been made of a model of a boundary layer consisting of a subsonic stream bounded on one side by a wall and on the other by a supersonic main stream. The subsonic stream was approximately uniform at the point where it first met the main stream, but it became progressively less uniform downstream of this point because of mixing with the main stream and the growth of the boundary layer at the wall. Particular attention is given to the pressure rise which takes place at the wall when a wedge is attached to it. It is found that the pressure begins to rise ahead of the apex of the wedge, and that the magnitude of this upstream effect increases as the Mach number of the secondary stream is reduced. A comparison between the measured values of the upstream effect, and the values predicted by a theory which has been advanced by Lighthill shows reasonable agreement." @default.
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- W1510230107 date "1954-10-01" @default.
- W1510230107 modified "2023-09-25" @default.
- W1510230107 title "CX. An experimental investigation of the interaction of a shock wave with a subsonic stream, bounded by a wall" @default.
- W1510230107 cites W1604306590 @default.
- W1510230107 doi "https://doi.org/10.1080/14786441008520517" @default.
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