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Propeller flow visualization techniquesPropeller flow visualization techniques were tested. The actual operating blade shape as it determines the actual propeller performance and noise was established. The ability to photographically determine the advanced propeller blade tip deflections, local flow field conditions, and gain insight into aeroelastic instability is demonstrated. The analytical prediction methods which are being developed can be compared with experimental data. These comparisons contribute to the verification of these improved methods and give improved capability for designing future advanced propellers with enhanced performance and noise characteristics.
Document ID
19820024796
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stefko, G. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Paulovich, F. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Greissing, J. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Walker, E. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Publication Information
Publication: NASA. Langley Research Center Flow Visualization and Laser Velocimetry for Wind Tunnels
Subject Category
Instrumentation And Photography
Accession Number
82N32672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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