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Numerical modeling of gas turbine cooled blades

Abstract

In contrast to methods that do not take into account multiconnectivity in a broad sense of this term, we develop mathematical models and highly effective combination (BIEM and FDM) numerical methods of calculation of stationary and quasi‐stationary temperature field of a profile part of a blade with convective cooling (from the point of view of realization on PC). The theoretical substantiation of these methods is proved by appropriate theorems. For it, converging quadrature processes have been developed and the estimations of errors in the terms of A. Ziqmound continuity modules have been received.


First Published Online: 14 Oct 2010

Keyword : multiconnected systems, method of the boundary integrated equations, splints, neural networks

How to Cite
Pashayev, A., Askerov, D., & Sadiqov, R. A. C. oqlu. (2005). Numerical modeling of gas turbine cooled blades. Aviation, 9(3), 9-18. https://doi.org/10.3846/16487788.2005.9635905
Published in Issue
Sep 30, 2005
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