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Spanwise loading distribution and wake velocity surveys of a semi-span wingThe spanwise distribution of bound circulation on a semi-span wing and the flow velocities in its wake were measured in a wind tunnel. Particular attention was given to documenting the flow velocities in and around the development tip vortex. A two-component laser velocimeter was used to make the velocity measurements. The spanwise distribution of bound circulation, three components of the time-averaged velocities throughout the near wake their standard deviations, and the integrated forces and moments on a metric tip as measured by an internal strain gage balance are presented without discussion.
Document ID
19820011290
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Felker, F. F., III
(NASA Ames Research Center Moffett Field, CA, United States)
Piziali, R. A.
((Army Aviation Research and Development Command Moffett Field, Calif., United States)
Gall, J. K.
(Informatics Inc. Moffett Field, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
A-8819
NASA-TM-84213
USAAVRADCOM-TR-81-A-1
Accession Number
82N19164
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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