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Scale-model studies for the improvement of flow patterns of a low-speed tunnelParameters affecting the performance of a scale model V/STOL wind tunnel were measured. These included: (1) static pressure variation around the closed tunnel circuit as affected by the application of various screens; (2) pressure rise and radial distribution of flow through the fan; (3) variation of screen parameters and screen location affecting the flow; and (4) effects of multiple screens on the velocity distribution in the fourth diffuser. In these tests the fan was driven through a long shaft by an externally situated 11,190-W (15-HP) motor equipped to turn at 4 speeds.
Document ID
19820009354
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barna, P. S.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-169413
Report Number: NASA-CR-169413
Accession Number
82N17228
Funding Number(s)
CONTRACT_GRANT: NSG-1563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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