Propellors in high-speed dives

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dc.contributor.author J. F. C. Conn
dc.contributor.author Love, E.M.
dc.date.accessioned 2014-10-21T12:03:35Z
dc.date.available 2014-10-21T12:03:35Z
dc.date.issued 1942
dc.identifier.other ARC/R&M-2040 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/1463
dc.description.abstract The performance of a variable-pitch, 3-bladed propellor has been calculated for conditions of fixed power absorption, fixed rotational speed and varying advance speed. Curves of efficiency and power-loss ratios are given to a base of V/a (advance speed/velocity of sound, Fig 1), together with thrust, torque grading and compressibility loss curves to a base of (radius) squared (Fig. 2). Increasing values of V/a (up to 0.85 or 600 m.p.h. at 21,000 ft.) representing the conditions of a high-speed dive, are accompanied by marked decreases in efficiency and under these conditions the thrust becomes negative over the tips of the blades. en_US
dc.language.iso en en_US
dc.publisher H. M. Stationery Office en_US
dc.relation.ispartofseries Aeronautical Research Committee Reports & Memoranda en_US
dc.title Propellors in high-speed dives en_US
dc.type Technical Report en_US


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