NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Rectangular subsonic jet flowfield studyThe flowfield of a rectangular jet with 2:1 aspect ratio was studied at an axial Reynolds number of 127,000, using a three-dimensional laser anemometer. The flowfield surveys resulted in mean velocity vector field plots and contour plots of the Reynolds stress tensor components for the major and minor axes. These data contribute substantially to currently available data of jet flowfields.
Document ID
19880029345
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morrison, Gerald L.
(Texas A&M Univ. College Station, TX, United States)
Tatterson, Gary B.
(Texas A & M University College Station, United States)
Swan, David H.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 87-2732
Accession Number
88A16572
Funding Number(s)
CONTRACT_GRANT: NAG1-630
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available