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- W2016121858 abstract "Narasimha and Sreenivasan mentioned that the interaction region appears to be insensitive to the corner deflection angle for supersonic flow. Here, this statement is corroborated for a low supersonic Mach number in conjunction with the work of Lu and Chung, which allows conclusions to be drawn concerning Mach number effects on the extent of the interaction region for turbulent expansion corner flows. In addition, an interaction region based on surface pressure fluctuations is illustrated" @default.
- W2016121858 created "2016-06-24" @default.
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- W2016121858 date "1998-06-01" @default.
- W2016121858 modified "2023-09-24" @default.
- W2016121858 title "Interaction Region of Turbulent Expansion-Corner Flow" @default.
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- W2016121858 doi "https://doi.org/10.2514/2.490" @default.
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