Computational and experimental study of heat transfer in rotating ribbed radial turbine cooling passages

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...

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Chi tiết về thư mục
Những tác giả chính:	Pearce, R, Ireland, P, He, L, McGilvray, M, Romero, E
Định dạng:	Conference item
Được phát hành:	American Society of Mechanical Engineers 2015

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