NASA NTRS ยท 19820031924
The three-dimensional boundary layer on a rotating helical blade
Abstract
The 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.
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Morris, P. J.. 1981-11-01. The three-dimensional boundary layer on a rotating helical blade. https://ntrs.nasa.gov/citations/19820031924
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