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An experimental investigation of the flow fields about delta and double-delta wings at low speedsLow speed wind tunnel analysis of flow fields about delta and double delta wings
Document ID
19660025758
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mc Mahon, M. C. (Wichita Univ. Wichita, KS, United States)
Wentz, W. H., Jr. (Wichita Univ. Wichita, KS, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-521
Report Number: NASA-CR-521
Accession Number
66N35048
Funding Number(s)
CONTRACT_GRANT: NGR-17-003-003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOW SPEED WIND TUNNEL
FLOW FIELD
DELTA WING

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