Effects of temperature distribution and level on heat transfer on a rotating free disk
Effects of temperature distribution and level on heat transfer on a rotating free disk
-
摘要: In gas turbine engines, with the existence of the intense forced convection and significant buoyancy effects, temperature distribution and level on turbine or compressor disks affect the heat transfer characteristics strongly. In this paper, numerical simulations were performed to analyze these influences for a free disk, with the laminar and turbulent flow respectively. The influences of temperature distribution on the heat transfer were observed by using incompressible cooling air, and temperature profiles of nth order monomial and polynomial were assumed on the disk. The analysis revealed that the heat transfer for two flow states on the free disk is determined by the exponent n of the monomial profile when specifying the rotating Reynolds number; for an arbitrary polynomial profile, the local Nusselt number can be deduced from results of monomial profiles. To study the effects of temperature level on heat transfer singly, monomial profiles were used and the local Nusselt number of compressible and incompressible cooling air were compared.And both for two flow states, the following conclusions could be drawn: the relative difference of local Nusselt number is mainly controlled by nondimensional local temperature difference, and almost independent of the monomial's coefficient C, exponent n and the rotating Reynolds number. Subsequently, a correction method for heat transfer of the free disk is presented and verified computationally, with which the local Nusselt number, obtained with a uniform and low temperature profile, can be revised by arbitrary distribution and high temperature magnitude.Abstract: In gas turbine engines, with the existence of the intense forced convection and significant buoyancy effects, temperature distribution and level on turbine or compressor disks affect the heat transfer characteristics strongly. In this paper, numerical simulations were performed to analyze these influences for a free disk, with the laminar and turbulent flow respectively. The influences of temperature distribution on the heat transfer were observed by using incompressible cooling air, and temperature profiles of nth order monomial and polynomial were assumed on the disk. The analysis revealed that the heat transfer for two flow states on the free disk is determined by the exponent n of the monomial profile when specifying the rotating Reynolds number; for an arbitrary polynomial profile, the local Nusselt number can be deduced from results of monomial profiles. To study the effects of temperature level on heat transfer singly, monomial profiles were used and the local Nusselt number of compressible and incompressible cooling air were compared.And both for two flow states, the following conclusions could be drawn: the relative difference of local Nusselt number is mainly controlled by nondimensional local temperature difference, and almost independent of the monomial's coefficient C, exponent n and the rotating Reynolds number. Subsequently, a correction method for heat transfer of the free disk is presented and verified computationally, with which the local Nusselt number, obtained with a uniform and low temperature profile, can be revised by arbitrary distribution and high temperature magnitude.
-
Key words:
- thermal boundary condition /
- temperature boundary condition /
- rotating disk /
- free disk
-
[1] CAO Yuzhang,TAO Zhi,XU Guoqiang,et al.Heat transfer of aero-engine[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2005.(in Chinese) [2] Baxter D C,Reynolds W C.Fundamental solution for heat transfer from nonisothermal flat plates[J].Journal of Aeronautical Sciences,1958,25(6):403-404. [3] Taylor R P,Coleman H W,Hosni M H,et al.Thermal boundary condition effects on heat transfer in the turbulent incompressible flat plate boundary layer[J].International Journal of Heat and Mass Transfer,1989,32(6):1165-1174. [4] Baughn J W, Saniei N.The effect of the thermal boundary condition on heat transfer from a cylinder in crossflow[J]. ASME Journal of Heat Transfer,1991,113(4):1020-1023. [5] Butler R J.The effects of the thermal boundary condition and turbulence on heat transfer from a cylinder,flat plate,and turbine blade using the transient shroud and heated-coating techniques .Davis:University of California at Davis,1995. [6] Butler R J, Baughn J W.The effect of the thermal boundary condition on transient method heat transfer measurements on a flat plate with a laminar boundary layer[J].ASME Journal of Heat Transfer,1996,118(4):831-837. [7] Dorfman L A.Influence of a radial temperature gradient on the heat transfer from a rotating disk[J].Izv Akad Nauk SSSR,Otd Tekh Nauk,1957(7):138-142. [8] Dorfman L A.Hydrodynamic resistance and the heat loss of rotating solids[M].Kemmer N,Trans.Edinbargh:Oliver and Boyd Ltd.,1963. [9] Owen J M,Rogers R H.Flow and heat transfer in rotating-disc systems: rotor-stator systems[M].Launton:Research Studies Press,1989. [10] LV Pin,WANG Chenming,ZHAO Xi,et al.Effect of temperature distribution on laminar heat transfer for free disk[J].Aeroengine,2010,36(4):8-11.(in Chinese) [11] Kim S Y,Han J C,Morrison G L.Local heat transfer in enclosed co-rotating disks with axial throughflow[J].ASME Journal of Heat Transfer,1994,116(1):66-72. [12] Soong C Y.Theoretical analysis for axisymmetric mixed convection between rotating coaxial disks[J]. International Journal of Heat and Mass Transfer,1996,39(8):1569-1583. [13] SUN Jining,TAO Zhi,DING Shuiting,et al.Numerical investigation of fluid flow and heat transfer characteristics within a rotating cavity with a high positioned axial inlet and a radial outlet[J].Journal of Aerospace Power,2002,17(5):586-590.(in Chinese) [14] Owen J M,Powell J.Buoyancy-induced flow in a heated rotating cavity .ASME GT2004-53210,2004. [15] TIAN Shuqing,TAO Zhi,DING Shuiting,et al.Investigation of flow and heat transfer instabilities in a rotating cavity with axial throughflow of cooling air .ASME GT2004-53525,2004. [16] ZHAO Xi,XU Guoqiang,TAO Zhi,et al.Effect of temperature level on heat transfer on a free disk with laminar flow[J].Journal of Aerospace Power,2010,25(3):503-508.(in Chinese) [17] CHEN Maozhang.Fundamentals of fluid dynamics[M].Beijing: Higher Education Press,2002.(in Chinese) [18] Eckert E R G,Drake R M.Analysis of heat and mass transfer[M].New York:McGraw-Hill,1972. -
点击查看大图
计量
- 文章访问数: 1577
- HTML浏览量: 168
- PDF量: 19
- 被引次数: 0

下载: