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Turbine endwall single cylinder programDetailed measurement of the flow field in front of a large-scale single cylinder, mounted in a wind tunnel is discussed. A better understanding of the three dimensional separation occuring in front of the cylinder on the endwall, and of the vortex system that is formed is sought. A data base with which to check analytical and numerical computer models of three dimensional flows is also anticipated.
Document ID
19820023762
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Langston, L. S.
(Connecticut Univ. Storrs, CT, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-169278
NAS 1.26:169278
Report Number: NASA-CR-169278
Report Number: NAS 1.26:169278
Accession Number
82N31638
Funding Number(s)
CONTRACT_GRANT: NSG-3238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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