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The NASA Lewis Research Center Water Tunnel FacilityA water tunnel facility specifically designed to investigate internal fluid duct flows has been built at the NASA Research Center. It is built in a modular fashion so that a variety of internal flow test hardware can be installed in the facility with minimal facility reconfiguration. The facility and test hardware interfaces are discussed along with design constraints for future test hardware. The inlet chamber flow conditioning approach is also detailed. Instrumentation and data acquisition capabilities are discussed. The incoming flow quality has been documented for about one quarter of the current facility operating range. At that range, there is some scatter in the data in the turbulent boundary layer which approaches 10 percent of the duct radius leading to a uniform core.
Document ID
19970022774
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wasserbauer, Charles A.
(NYMA, Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
E-10756
NASA-CR-4777
NAS 1.26:4777
Report Number: E-10756
Report Number: NASA-CR-4777
Report Number: NAS 1.26:4777
Accession Number
97N23219
Funding Number(s)
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 523-36-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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