NASA NTRS · 19950065328
Microsensor Hot-Film Anemometer
Abstract
Improved hot-film anemometer developed for making high-bandwidth turbulence measurements in moderate-enthalpy supersonic and hypersonic flows (e.g., NASP inlets and control surfaces, HSCT jet exhaust). Features include low thermal inertia, ruggedness, and reduced perturbation of flow.
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Mcginley, Catherine B., Stephens, Ralph, Hopson, Purnell, Bartlett, James E., Sheplak, Mark, Spina, Eric F.. 1995-04-01. Microsensor Hot-Film Anemometer. https://ntrs.nasa.gov/citations/19950065328
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