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Turbine endwall single cylinder programMeasurements of the flow field in front of a large-scale single cylinder, mounted in a wind tunnel are discussed. Static pressures on the endwall and cylinder surfaces, extensive five-hole probe pressures in front of and around the cylinder, and velocity fluctuations using a hot-wire probe where the flow is steady enough to yield meaningful results are included.
Document ID
19830011490
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Langston, L. S.
(Connecticut Univ. Storrs, CT, United States)
Eckerle, W. A.
(Connecticut Univ. Storrs, CT, United States)
Date Acquired
September 4, 2013
Publication Date
March 18, 1983
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:170008
NASA-CR-170008
Report Number: NAS 1.26:170008
Report Number: NASA-CR-170008
Accession Number
83N19761
Funding Number(s)
CONTRACT_GRANT: NSG-3238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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