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Laser transit anemometer experiences in supersonic flowThe purpose of this paper is to present examples of velocity measurements obtained in supersonic flow fields with the laser transit anemometer system. Velocity measurements of a supersonic jet exhausting in a transonic flow field, a cone boundary survey in a Mach 4 flow field, and a determination of the periodic disturbance frequencies of a sonic nozzle flow field are presented. Each of the above three cases also serves to illustrate different modes of laser transit anemometer operation. A brief description of the laser transit anemometer system is also presented.
Document ID
19930068160
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hunter, William W., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Humphreys, William M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1988
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: Supersonic Tunnel Association, Semiannual Meeting
Location: Preston
Country: United Kingdom
Start Date: October 11, 1988
End Date: October 12, 1988
Sponsors: Supersonic Tunnel Association
Accession Number
93A52157
Distribution Limits
Public
Copyright
Other

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