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Blade-vortex interactionA conformal transformation and discrete vortex dynamics are used to calculate the interaction of a blade with vortices drifting with the free stream. An unsteady Kutta condition is employed to dictate the strength of vortices shed at the trailing edge. Instantaneous pressure distributions are calculated and compared with earlier experimental and analytical data.
Document ID
19870037697
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Poling, David R. (Boeing Vertol Co. Philadelphia, PA, United States)
Dadone, Leo (Boeing Vertol Co. Philadelphia, PA, United States)
Telionis, Demetri P. (Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-0497
Report Number: AIAA PAPER 87-0497
Accession Number
87A24971
Distribution Limits
Public
Copyright
Other

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