Abstract:The high performance of aircraft turbine engines-mainly oriented towards economy in civil engines and towards performance, economy and off-design reliability in military applications-depends on the correct design of gas flows in the engine. Today, this is mainly done by numerical computer simulation instead of the much more costly experimentation with hardware. The working group undertook to analyse the quality of computer codes in use and to show ways for improvement. Many discrepancies between codes were det… Show more
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