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Rectangular subsonic jet flow field measurementsFlow field measurements are presented of 3 subsonic rectangular cold air jets. The 3 cases presented had aspect ratios of 1 x 2, 1 x 4 at a Mach number of 0.09 and an aspect ratio of 1 x 2 at a Mach number of 0.9. All measurements were made using a 3-D laser Doppler anemoneter system. The presented data includes the mean velocity vector, all Reynolds stress tensor components, turbulent kinetic energy and velocity correlation coefficients. The data is presented in tabular and graphical form. No analysis of the measured data or comparison to other published data is made. All tabular data are available in ASCII format on MS-DOS compatible disks.
Document ID
19900001939
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
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-185962
NAS 1.26:185962
Accession Number
90N11255
Funding Number(s)
CONTRACT_GRANT: NAG1-630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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