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Turbulence Measurement in Transonic FlowTwo instrumentation systems are presently practical to use in turbulence measurements. The laser velocimeter can measure fluctuating velocities while the hot-wire anemometer, in principle, can be used to obtain both kinematic and thermodynamic fluctuations. In addition, the hot-wire anemometer gives an analog signal output that is convenient for use in time-space correlation studies and spectral analyses. The laser velocimeter has been used successfully in all flow regimes, whereas the hot wire has not been exploited in transonic flows, where the wire response has not been well-understood. The purpose of this Note is to examine the response and calibration of a constant-temperature, hot- wire anemometer in transonic flow and to present turbulence measurements, obtained in a transonic boundary layer.
Document ID
19990054114
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Rose, William C.
(NASA Ames Research Center Moffett Field, CA United States)
McDaid, Edward P.
(Washington Univ. Seattle, WA United States)
Date Acquired
August 19, 2013
Publication Date
September 1, 1977
Publication Information
Publication: AIAA Journal
Publisher: American Inst. of Aeronautics and Astronautics
Volume: 15
Issue: 9
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Aerodynamic Testing
Location: Arlington, TX
Country: United States
Start Date: June 7, 1976
End Date: June 9, 1976
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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