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Experimental and Theoretical Investigation of Wind Tunnel Geometry, Emphasizing Factors Pertinent to V/STOL Vehicles Testing Progress Report No. 2, Mar. 16 - Sep. 15, 1965Powered rotor installation, tunnel internal flow analysis using vortex ring, and flow field calculation of highly loaded systems in free air for V/STOL vehicles test program
Document ID
19660007797
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Joppa, R. G. (Washington Univ. Seattle, WA, United States)
Date Acquired
August 3, 2013
Publication Date
January 15, 1966
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-CR-70331
Report Number: NASA-CR-70331
Accession Number
66N17086
Funding Number(s)
CONTRACT_GRANT: NGR-48-002-010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VORTEX RING
FLOW FIELD
WIND TUNNEL APPARATUS
V/STOL AIRCRAFT

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