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Experimental and theoretical investigation of wind tunnel geometry, emphasizing factors pertinent to V/STOL vehicle testing Progress report, 16 Mar. - 15 Sep. 1968Progress on experimental program using jet flapped wing model in wind tunnel facilities for testing V/STOL aircraft
Document ID
19690002198
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Joppa, R. G. (Washington Univ. Seattle, WA, United States)
Date Acquired
August 5, 2013
Publication Date
September 1, 1968
Subject Category
Facilities, Research, And Support
Report/Patent Number
PR-8
NASA-CR-66719
Report Number: PR-8
Report Number: NASA-CR-66719
Accession Number
69N11529
Funding Number(s)
CONTRACT_GRANT: NGR-48-002-010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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