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- W624578416 abstract "The position of the sonic line and the pressure distribution over the wedge have been calculated from the density fields measured with a Mach-Zehnder interferometer. For a given wedge, identical pressure distributions are found over a considerable range of supersonic flows. These results suggest simple formulas giving the drag coefficient for each wedge angle which are expected to hold in most of the transonic speed range." @default.
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- W624578416 date "1952-04-01" @default.
- W624578416 modified "2023-09-23" @default.
- W624578416 title "Shock-Tube Studies of Transonic Flow over Wedge Profiles" @default.
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- W624578416 doi "https://doi.org/10.2514/8.2242" @default.
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