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Experimental and Theoretical Investigation of Wind Tunnel Geometry, Emphasizing Factors Pertinent to V/STOL Vehicles Testing Progress Report No. 3, Sep. 16, 1965 - Mar. 15, 1966Wind tunnel tests to measure converging flow field effects on V/STOL models
Document ID
19660020004
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
June 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-75822
Report Number: NASA-CR-75822
Accession Number
66N29294
Funding Number(s)
CONTRACT_GRANT: NGR-48-002-010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
FLOW FIELD
V/STOL AIRCRAFT

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