Computational and experimental study of heat transfer in rotating ribbed radial turbine cooling passages
This study investigates the effect of rotation on the Nusselt number distribution within ribbed radial turbine cooling passages representative of systems used in current jet engines. The results are unusual in that the cooling passage length to diameter ratio is engine representative and full distri...
المؤلفون الرئيسيون: | Pearce, R, Ireland, P, He, L, McGilvray, M, Romero, E |
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التنسيق: | Conference item |
منشور في: |
American Society of Mechanical Engineers
2015
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مواد مشابهة
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Computational study of the effect of inlet velocity profile and rib orientation on heat transfer in rotating ribbed radial turbine cooling passages
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