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RESEARCH PAPERS: Papers From Symposium on Three-Dimensional Flow in Turbomachines

A Nearly Three-Dimensional Intrablade Computing System for Turbomachinery

[+] Author and Article Information
R. A. Novak

Aerodynamics Aircraft Engine Group, General Electric Co., Lynn, Mass.

R. M. Hearsey

Hearsey Technology, Allentown, Pa.

J. Fluids Eng 99(1), 154-166 (Mar 01, 1977) (13 pages) doi:10.1115/1.3448517 History: Received January 05, 1976; Online October 12, 2010

Abstract

The structure of a computing system for bladed or unbladed turbomachinery passages is described and discussed. The system, in an overall sense, is modeled after the work of Wu, and is comprised of two coordinated computer programs, one providing solutions on rotationally symmetric blade-to-blade surfaces and the second on streamsheets roughly parallel to the blades. Both approaches utilize streamline curvature techniques.

Copyright © 1977 by ASME
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