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RESEARCH PAPERS

Design Comments and Experimental Results for Cavitation-Resistant Inducers up to 40,000 Suction Specific Speed

[+] Author and Article Information
M. K. Wright

Rotating Machinery Section, Design and Development Dept., Rockets Division, Textron’s Bell Aerosystems Co., Buffalo, N. Y.

J. Eng. Power 86(2), 176-180 (Apr 01, 1964) (5 pages) doi:10.1115/1.3677571 History: Received January 16, 1963; Online January 10, 2012

Abstract

General geometric design considerations for cavitation resistant inducers are discussed, particularly those related to the “trial and error” type not covered by the textbook approach. A general correlation of four dimensionless cavitation parameters is developed. Experimental data for typical rocket engine pumps are given where suction specific speed values up to 40,000 are obtained. Finally, several schemes are given for augmenting the cavitation resistance.

Copyright © 1964 by ASME
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