Heat transfer in high-pressure compressor gas turbine internal air systems: A arotating disc-cone cavity with axial throughflow

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作者
Alexiou, A.
Hills, N.J.
Long, Christopher
Turner, A.B.
Millward, J.A.
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[1] Thermo-Fluid Mechanics Res. Centre, School of Engineering, University of Sussex, Brighton, Sussex, United Kingdom
[2] Rolls-Royce Plc., Derby, United Kingdom
[3] Thermo-Fluid Mechanics Res. Centre, School of Engineering, University of Sussex, Brighton, BN1 9QT, Sussex, United Kingdom
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页码:299 / 328
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