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Rectangular subsonic jet flow field measurementsFlow field measurements of three subsonic rectangular cold air jets are presented. The three cases had aspect ratios of 1x2, 1x4 at a Mach number of 0.09 and an aspect ratio of 1x2 at a Mach number of 0.9. All measurements were made using a 3-D laser Doppler anemometer system. The data includes the mean velocity vector, all Reynolds stress tensor components, turbulent kinetic energy and velocity correlation coefficients. The data are presented in tabular and graphical form. No analysis of the measured data or comparison to other published data is made.
Document ID
19900012282
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morrison, Gerald L.
(Texas A&M Univ. College Station, TX, United States)
Swan, David H.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:181925
NASA-CR-181925
TL-89-JETS-GLM-1
Report Number: NAS 1.26:181925
Report Number: NASA-CR-181925
Report Number: TL-89-JETS-GLM-1
Accession Number
90N21598
Funding Number(s)
CONTRACT_GRANT: NAG1-630
PROJECT: RTOP 505-61-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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