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RESEARCH PAPERS

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

[+] Author and Article Information
Siu Shing Tong, W. T. Thompkins

Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Mass. 02139

J. Eng. Power 105(2), 369-376 (Apr 01, 1983) (8 pages) doi:10.1115/1.3227425 History: Received December 15, 1981; Online September 28, 2009

Abstract

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 precompression type rotor designs.

Copyright © 1983 by ASME
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