Optimization of Micro Compressor Blades Using CFD Analysis and Artificial Intelligence
Keyword(s):
This paper describes a robust design method for turbo machinery components. The method which uses a Navier Stokes (NS) solver, an Artificial Neural Network (ANN) and a Genetic Algorithm (GA) is applied to optimize radial micro compressor blades. Higher efficiency, less divergence from the design mass flow and smoother Mach number distributions are considered as objectives of the optimization.
2013 ◽
Vol 347-350
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pp. 3537-3540
2010 ◽
Vol 458
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pp. 212-217
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2012 ◽
Vol 542-543
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pp. 1394-1397
2014 ◽
Vol 902
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pp. 431-436
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2019 ◽
Vol 8
(10)
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pp. 3415-3421
2019 ◽
Vol 232
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pp. 1418-1429
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