跨声压气机动静干涉效应的数值研究

毛明明; 宋彦萍; 王仲奇

跨声压气机动静干涉效应的数值研究

哈尔滨工业大学能源科学与工程学院, 哈尔滨 150001

基金项目: 国家自然科学基金(No.50646021); 高等学校博士学科点专项科研基金(No.20060213007)

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出版历程
- 收稿日期: 2007-01-25
- 修回日期: 2007-04-20
- 刊出日期: 2007-09-28

Numerical research on influence of rotor-stator interactions in transonic compressor

School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

摘要

摘要: 采用数值方法对一轴流跨声压气机在设计点的非定常流场进行了模拟, 对级内动静干涉进行了深入分析, 研究了尾迹和位势作用等对动静叶表面气动负荷的影响.计算结果表明:在压气机中, 上游动叶的尾迹等对静叶通道内部流动, 叶片表面静压的波动, 以及边界层流动损失的发生、发展和输运产生明显的影响, 需要在设计中加以考虑.
- 航空、航天推进系统 /
- 非定常流动 /
- 跨声压气机 /
- 动静干涉 /
- 尾迹 /
- 位势作用
Abstract: The unsteady flow field of a single stage axial transonic compressor at a design point was simulated numerically,and an in-depth analysis of rotor-stator interaction was performed.Moreover,the influences of upstream wakes and potential effects on downstream blade loading distributions were investigated extensively.The results indicate that,under stage environment,upstream wakes have obvious influences on generation,evolution and transportation of flow losses,and also on loading distributions of downstream blade.Therefore,consideration shall be given to this effect in the design of turbomachinery.
- aerospace propulsion system /
- unsteady flow /
- transonic compressor /
- rotor-stator interaction /
- wake /
- potential effect

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参考文献(19)

[1]	张文龙,袁巍,张健,等.压气机二维叶栅涡脱落的数值模拟[J].航空动力学报,2002,17(5):556-560.ZHANG Wenlong,YUAN Wei,ZHANG Jian,et al.Numerical simulation of trailing edge vortex shedding in a 2-D compressor cascade[J].Journal of Aerospace Power,2002,17(5):556-560.
[2]	Walker G J.The turbulent boundary layer on an axial compressor blade[R].ASME Paper 82-GT-52.
[3]	Pfeil H,Herbst R,Schr(o)der T.Investigation of the laminar-turbulent transition of boundary layers disturbed by wakes[J].Journal of Engineering for Power.1983,105:130-137.
[4]	Hodson H P.Boundary layer and loss measurements on the rotor on an axial flow turbine[R].ASME Paper 83-GT-4.
[5]	Schulte V,Hodson H P.Prediction of the becalmed region for LP turbine profile design[R].ASME Paper 97-GT-398.
[6]	Poensgen C,Gallus H E.Three-dimensional wake decay inside of a compressor cascade and its influence on the downstream unsteady flow field[R].ASME Paper 90-GT-21.
[7]	Gorell S E,Copenhaver W W,Chriss R M.Effects of upstream wakes on the performance of a transonic compressor stage[C]∥13th ISABE Conference,Sept.,Paper No.97-7070,Chattanooga:1997.
[8]	Chriss R M,Copenhaver W W,Gorrell S E.The effects of blade-row spacing on the flow capacity of a transonic rotor[R].ASME Paper 99-GT-209.
[9]	Gorell S E,Okiishi T H,Copenhaver W W.Stator-rotor interactions in a transonic compressor:part 1:effect of blade-row spacing on performance[R].ASME Paper 2002-GT-30494.
[10]	Gorell S E,Okiishi T H,Copenhaver W W.Stator-rotor Interactions in a transonic compressor:part 2:description of a loss producing mechanism[R].ASME Paper 2002-GT-30494.
[11]	Gorrell S E,Car D,Puterbaugh S L,et al.An investigation of wake-shock interactions in a transonic compressor with DPIV and time-accurate CFD[R].ASME paper 2005-GT-69107.
[12]	宁卫,刘前智,姚吉先,等.跨声速压气机动静叶排相干的三维非定常流动数值分析[J].航空动力学报.1996,11(4):161-164.NING Wei,LIU Qianzhi,YAO Jixian,et al.Numerical analysis of 3-D unsteady flow induced by rotor/stator interaction inside a transonic compressor stage[J].Journal of Aerospace Power,1996,11(4):161-164.
[13]	刘前智,周新海.单级跨声速压气机三维非定常粘性流动计算[J].航空动力学报.2000,15(1):12-16.LIU Qianzhi,ZHOU Xinhai.Computation of 3-D unsteady viscous flow in transonic compressor stage[J].Journal of Aerospace Power,2000,15(1):12-16.
[14]	吴先鸿,陈矛章.非定常动静叶干涉作用的二维数值模拟[J].航空动力学报.1998,13(2):123-128.WU Xianhong,CHEN Maozhang.Two-dimensional numerical simulation of unsteady rotor/stator interaction[J].Journal of Aerospace Power,1998,13(2):123-128.
[15]	Chen M Z,Wu X H.Vortex simulation of rotor/stator interaction in turbomachinery[R].ASME Paper 98-GT-15,1998
[16]	周盛,韩振学,孟庆国.计算流体力学在吸气式推进领域中的某些应用[J].空气动力学学报.1998,16(1):97-107.ZHOU Sheng,HAN Zhenxue,MENG Qingguo.Some applications of computational fluid dynamics in the field of air breathing propulsion[J].Acta Aerodynamica Sinica.1998,16(1):97-107.
[17]	侯安平,周盛.轴流式叶轮机时序效应的机理探讨[J].航空动力学报.2003,18(1):197-202.HOU Anping,ZHOU Sheng.Probe into the mechanism of clocking effect in trubmachinery[J].Journal of Aerospace Power.2003,18(1):197-202.
[18]	邹正平,宁方飞,刘火星,等.雷诺数对涡轮叶栅流动的影响[J].工程热物理学报.2004,25(2):216-219.ZOU Zhengping,NING Fangfei,LIU Huoxing,et al.Effect of reynolds number on turbine cascade flow[J].Journal of Engineering Thermophysics,2004,25(2):216-219.
[19]	邹正平,叶建,张永信,等.非定常流动对叶片表面负荷分布影响的数值模拟研究[J].燃气涡轮试验与研究.2006,19(1):21-26.ZOU Zhengping,YE Jian,ZHANG Yongxin,et al.Numerical simulation of unsteady flow effects on turbine blade loading distributions[J].Gas Turbine Experiment and Research,2006,19(1):21-26.