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On wings of circular designPrandtl's method of sources and sinks for air foils is used to investigate the aerodynamics of circular wings in constant flow. Lift distribution, total lift, and pitching moment are investigated as well as the influence of changes in the angle of attack.
Document ID
19800011747
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kinner, W. (NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-75505
Report Number: NASA-TM-75505
Accession Number
80N20229
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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