A Contribution to Designing a Radial Flow Gas Turbine Stage PUBLIC ACCESS

[+] Author Affiliations
F. S. Bhinder

Hatfield Polytechnic, Hatfield, Herts, UK

Paper No. 90-GT-187, pp. V001T01A058; 8 pages
  • ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Brussels, Belgium, June 11–14, 1990
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7904-7
  • Copyright © 1990 by ASME


The performance of a radial inward flow gas turbine stage depends on the design of the rotor as well as that of the casing. The paper describes a simple procedure for designing the complete stage comprising a rotor and a single entry nozzle-less volute casing. The rotor design follows a prescribed mean stream velocity distribution in a step by step manner and the casing design uses the radial equilibrium together with the conservation of mass energy and momentum equations.

Copyright © 1990 by ASME
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