Numerical Investigation on Heat Transfer in a Rotating Cavity with Axial Throughflow Cooling Air
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Numerical Investigation on Heat Transfer in a Rotating Cavity with Axial Throughflow Cooling Air
Vol. 20, Issue 4, (2005)
作者机构:
北京航空航天大学航空发动机气动热力重点实验室,北京,100083
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Published:2005
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TIAN Shu-qing, TAO Zhi, DING Shui-ting, et al. Numerical Investigation on Heat Transfer in a Rotating Cavity with Axial Throughflow Cooling Air[J]. 2005, 20(4).
DOI:
TIAN Shu-qing, TAO Zhi, DING Shui-ting, et al. Numerical Investigation on Heat Transfer in a Rotating Cavity with Axial Throughflow Cooling Air[J]. 2005, 20(4).DOI:
Numerical Investigation on Heat Transfer in a Rotating Cavity with Axial Throughflow Cooling Air
To investigate the heat transfer in heated rotating cavities with axial throughflow cooling air
numerical simulations have been carried out based on the time-independent incompressible equations in rotating system.The effects of unstable flow and various forces on heat transfer were studied
and the heat transfer coefficient variations with Reynolds number and Rayleigh number were calculated.The results show that the heat transfer in a rotating cavity with axial throughflow cooling air is enhanced with the increase of the inertia force and buoyancy force
and is weakened with the increase of the Coriolis force.The heat transfer coefficient rises with Reynolds number
and varies slightly with the increase of Rayleigh number.The sudden enhancement of heat transfer is caused by the penetration of cooling air through the disc cavity.