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Temperature and velocity field of the two-dimensional transverse hot-air jet in a freestream flow.Experimental investigation of the low subsonic, two-dimensional transverse hot-air jet. In the study jet-to-freestream angles of 90, 120, 135, and 150 deg and jet-to-freestream velocity ratios of 5, 10, and 20 were investigated. In the tests the jet velocity and temperature fields were measured using a temperature-compensated hot-wire anemometer. Photographs of the flowfield were also made. The tests results are compared with the available data and analysis. Results indicate a relatively minor deflection of the freestream by the jet and the presence of a large separated flow region behind the jet.
Document ID
19720041564
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tatom, J. W.
Cooper, M. A.
Hayden, T. K.
(Vanderbilt University Nashville, Tenn., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 72-292
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: San Antonio, TX
Start Date: April 10, 1972
End Date: April 12, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A25230
Funding Number(s)
CONTRACT_GRANT: NGR-43-002-034
Distribution Limits
Public
Copyright
Other

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