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Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft : Phase 2: Wind tunnel tests, analysis, and prediction techniques. Volume 2: Wind tunnel test and basic dataA research program has been conducted to determine the degree of cruise drag correlation on the C-141A aircraft between predictions based on wind tunnel test data, and flight test results. Information is presented on the wind tunnel test program and basic aerodynamic data on the C-141A wind-tunnel model used in the correlation studies.
Document ID
19740010567
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Macwilkinson, D. G.
(Lockheed-Georgia Co. Marietta, GA, United States)
Blackerby, W. T.
(Lockheed-Georgia Co. Marietta, GA, United States)
Paterson, J. H.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Publication Information
Publisher: NASA
Subject Category
Aircraft
Report/Patent Number
LG73ER0058-VOL-2
NASA-CR-2334
Report Number: LG73ER0058-VOL-2
Report Number: NASA-CR-2334
Accession Number
74N18680
Funding Number(s)
CONTRACT_GRANT: NAS1-10045
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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