A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller

[+] Author and Article Information
M. L. Celestina, R. A. Mulac

Sverdrup Technology, Inc.

J. J. Adamczyk

NASA Lewis Research Center, Cleveland, OH 44135

J. Turbomach 108(2), 187-193 (Oct 01, 1986) (7 pages) doi:10.1115/1.3262036 History: Received January 27, 1986; Online November 09, 2009


This paper presents the results of a numerical simulation of the time-averaged inviscid flow field through the blade rows of a multiblade row turboprop configuration. The governing equations are outlined along with a discussion of the solution procedure and coding strategy. Numerical results obtained from a simulation of the flow field through a modern high-speed turboprop will be shown.

Copyright © 1986 by ASME
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