Design of Turbomachinery Blading in Transonic Flows by the Circulation Method

[+] Author and Article Information
T. Q. Dang

Department of Mechanical/Aerospace Engineering, Syracuse University, Syracuse, NY 13244

J. Turbomach 114(1), 141-146 (Jan 01, 1992) (6 pages) doi:10.1115/1.2927977 History: Received August 01, 1990; Online June 09, 2008


The newly developed three-dimensional design technique for turbomachinery blading based on the circulation method has been successfully extended into the transonic flow regime. The main task involves replacing the classical Fourier series expansion technique by a finite-volume method. Calculations were carried out for the design of infinitely thin cascaded blades in transonic flows, including shocked and shock-free cascaded blades.

Copyright © 1992 by The American Society of Mechanical Engineers
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