Browsing Aeronautical Research Council Reports & Memoranda by Author "E. L. Hartley"

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Tests concerning novel designs of blades for axial compressors Part 1 blades designed for increased work at root and tip Part 2 blades designed to operate in a parabolic axial velocity distribution

S. J. Andrews; R. A. Jeffs; E. L. Hartley (1951)

Investigation of the flow between the blade rows in a research compressor with conventional Half-Vortex blades have shown a rapid stage-to,stage build-up of the annulus boundary layer. The axial velocity distribution under ...

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