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- W2019928235 abstract "Hot-wire anemometer measurements of the turbulence parameters were made in a 3.5-in. diameter free jet at exit Mach numbers between 0.2 and 0.7 and Reynolds numbers (based on jet rad.) between 192 000 and 725 000. The results of these measurements show that (1) the intensity of turbulence is a maximum at a distance of approximately 1 jet rad. from the jet center line and decreases with increasing Mach and/or Reynolds number, and (2) the lateral and longitudinal scales of turbulence are nearly independent of Mach and/or Reynolds number and vary proportionally with distance from the jet nozzle. The lateral scale is much smaller than the longitudinal and does not vary with distance from the center line, while the longitudinal scale is a maximum at a distance from the center line of about 0.7 to 0.8 of the jet rad." @default.
- W2019928235 created "2016-06-24" @default.
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- W2019928235 date "1956-07-01" @default.
- W2019928235 modified "2023-09-27" @default.
- W2019928235 title "Measurements of Turbulence in a Subsonic Air Jet" @default.
- W2019928235 doi "https://doi.org/10.1121/1.1905102" @default.
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