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The three-dimensional boundary layer on a rotating helical bladeThe laminar boundary layer on a twisted helical blade is considered. The blade geometry is the same as that proposed by Horlock and Wordsworth (1965). However, the blade is twisted about the leading edge in the manner described by Miyake and Fujita (1974). The flow may be considered to be the analog, in a rotating reference frame, of the flat-plate boundary layer in a stationary frame. It is shown that a coordinate system which is orthogonal in the blade surface may be developed. With the appropriate scaling of the dependent variables a solution for the boundary layer flow is readily obtained. The systems of ordinary differential equations for the stream function of the primary flow and the cross-flow are solved numerically.
Document ID
19820031924
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Morris, P. J.
(Pennsylvania State University University Park, PA, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1981
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 112
Subject Category
Aerodynamics
Accession Number
82A15459
Funding Number(s)
CONTRACT_GRANT: NSG-3265
Distribution Limits
Public
Copyright
Other

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