A computational tool for the design and optimization of supersonic turbines with application on turbopump rocket engines
Turbo-machinery design is clearly about making many decisions often under uncertainty and with multiple conflicting objectives. In this work, a computational tool has been developed to assist in the preliminary design optimization of supersonic turbines with application on turbopump rocket engines....
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2012
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3218 |