Genetic algorithm for preliminary design optimisation of high-performance axial-flow compressors
This work presents an approach to optimise the preliminary design of high-performance axial-flow compressors. The preliminary design within the Gas Turbine Group at ITA, is carried on with an in-house computational program based upon the streamline curvature method, using correlations from the liter...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2011
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1969 |