A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller
- 1 October 1986
- journal article
- Published by ASME International in Journal of Turbomachinery
- Vol. 108 (2) , 187-193
- https://doi.org/10.1115/1.3262036
Abstract
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.Keywords
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