Journal
EXPERIMENTS IN FLUIDS
Volume 56, Issue 12, Pages -Publisher
SPRINGER
DOI: 10.1007/s00348-015-2084-6
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Funding
- Australian Research Council
- USA Office of Naval Research
- Directorate For Engineering
- Div Of Chem, Bioeng, Env, & Transp Sys [1437851] Funding Source: National Science Foundation
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Multi-element hot-wire anemometry was used to measure spanwise vorticity fluctuations in turbulent boundary layers. Smooth wall boundary layer profiles, with very good spatial and temporal resolution, were acquired over a Karman number range of 2000-12,700 at the Melbourne Wind Tunnel at the University of Melbourne and the University of New Hampshire's Flow Physics Facility. A custom hot-wire probe was necessary to simultaneously obtain velocity and spanwise vorticity measurements centered at a fixed point in space. A custom calibration/processing scheme was developed to utilize single-wall-parallel wires to optimize the accuracy of the measured wall-normal velocity fluctuations derived from the sensor's x-array.
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