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Aerodynamic Development of a Radial Compressor for a 10-kw Turboalternator FREE

[+] Author Affiliations
Colin Rodgers

International Harvester Co., San Diego, CA

Paper No. 70-WA/GT-7, pp. V001T01A006; 7 pages
doi:10.1115/70-WA/GT-7
From:
  • ASME 1970 Winter Annual Meeting: GT Papers
  • ASME 1970 Winter Annual Meeting: GT Papers
  • New York, New York, USA, November 29–December 3, 1970
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-8004-3
  • Copyright © 1970 by ASME

abstract

The aerodynamic development of a small high-speed radial compressor for the US Army 10-kw turboalternator is discussed, including initial performance deficiencies arising from blade contour discrepancies. Design performance requirements were attained by correcting these discrepancies and subsequently were exceeded with further geometry refinements. Aerodynamic testing included an investigation concerning the effect of shroud axial clearance on compressor performance and showed that abradable shrouds are desirable for small compressors.

Copyright © 1970 by ASME
Topics: Compressors
This article is only available in the PDF format.

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