A Design Calculation Procedure for Shock-Free or Strong Passage Shock Turbomachinery Cascades PUBLIC ACCESS

[+] Author Affiliations
Siu Shing Tong, W. T. Thompkins, Jr.

Massachusetts Institute of Technology, Cambridge, MA

Paper No. 82-GT-220, pp. V001T01A073; 12 pages
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7956-6
  • Copyright © 1982 by ASME


A previously described inviscid design technique has been substantially improved to allow the generation of either shock free, weak shock or low total pressure loss supersonic rotor cascade designs. Improvements have been introduced in inflow-outflow boundary conditions, imposition of geometric constraints and in shock pressure rise specifications. Calculation examples are presented for pre-compression type rotor designs.

Copyright © 1982 by ASME
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