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The phenomenon of dynamic stallThe general features of dynamic stall on oscillating airfoils are explained in terms of the vortex shedding phenomenon, and the important differences between static stall, light dynamic stall, and deep stall are described. An overview of experimentation and prediction techniques is given.
Document ID
19810011501
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mccroskey, W. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
A-8464
NASA-TM-81264
Report Number: A-8464
Report Number: NASA-TM-81264
Accession Number
81N20029
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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