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The investigation of the flow about general fuselage shapes at high angles of attackWater tunnel visualization of the flow about bodies at high angles of attack was done. Wind tunnel tests on a series of models with non-circular cross sections are reported.
Document ID
19830005796
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clarkson, M. H. (Florida Univ. Gainesville, FL, United States)
Date Acquired
September 4, 2013
Publication Date
December 14, 1982
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:169611
NASA-CR-169611
Report Number: NAS 1.26:169611
Report Number: NASA-CR-169611
Accession Number
83N14067
Funding Number(s)
CONTRACT_GRANT: NCC2-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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