Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet
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Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet
Vol. 22, Issue 8, (2007)
作者机构:
南京航空航天大学高新技术研究院,南京,210016
作者简介:
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DOI:
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Published:2007
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WANG Suo-fang, ZHU Qiang-hua, ZHANG Yu, et al. Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet[J]. 2007, 22(8).
DOI:
WANG Suo-fang, ZHU Qiang-hua, ZHANG Yu, et al. Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet[J]. 2007, 22(8).DOI:
Numerical studies of heat transfer in a rotor-stator cavity with different radial positions of pre-swirl inlet
The three-dimensional numerical simulations of heat transfer in a rotor-stator cavity with pre-swirl nozzles at different radial positions in the stator were conducted in this paper.The standard k-ε turbulence model and unstructured grid were applied with the purpose of investigating the heat transfer characteristics.Under the constant mass flow rate and the different radial position of the pre-swirl nozzles
the outflow temperature and the effect of heat transfer on the rotor are greatly affected by the different rotational Reynolds number
pre-swirl angle and rotor-stator gap.The results show that the heat transfer of the rotor is enhanced with the increase of the rotational Reynolds number or the decrease of the rotor-stator gap.When the pre-swirl nozzles were moved out along the radial direction
the temperature difference between the inlet and the outlet and the averaged Nusselt number take on up-down tendency
that is
exists a optimum radial position of the pre-swirl nozzles.
Experimental study on heat transfer in rotor-stator cavity with high-positioned pre-swirl inflow
Heat transfer characteristics of axi-symmetrical nozzle and RS nozzle
Heat transfer characteristics of expander cycle thrust chamber
Flow and Heat Transfer in a Pre-Swirl Rotor-Stator Cavity under High Rotational Reynolds Number
Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle
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