Int. J. Simul. Multisci. Des. Optim.
Volume 5, 2014
|Number of page(s)||14|
|Published online||14 March 2014|
Evolutionary numerical simulation approach for design optimization of gas turbine blade cooling channels
Department of Industrial Engineering and Management Systems, University of Central Florida, Orlando, Florida
* e-mail: firstname.lastname@example.org
Accepted: 13 January 2014
Gas turbine blade cooling system design is a multidisciplinary, iterative and often tedious task involving complex relationships among multiple design objectives. Typical blade design requires a broad range of expertise in the materials, structural, heat transfer, and cost optimization disciplines. The multiple objectives involved are often conflicting and must be solved simultaneously with equal importance. The traditional approaches researchers scalarize the multiple objectives into a single objective using a weight vector, thus transforming the original multiple objective problem into a single objective problem. This research addresses the shortcomings of existing traditional approaches of the optimization of blade cooling configuration design.
Key words: Multiobjective / Optimization / Evolutionary / Numerical simulation / Gas turbine / Blade cooling channel / Ribs
© N.R. Nagaiah, C.D. Geiger, Published by EDP Sciences, 2014
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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