期刊文献+

离心压气机确定应力场分析 被引量:4

Analysis of deterministic stresses in a centrifugal compressor
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摘要 采用定常和非定常数值模拟技术,研究了某跨声离心压气机内的固有非定常流动.对比分析了定常流场和非定常时均流场之间的差别,着重分析了通道内确定应力的分布规律以及交界面确定应力的分布特点.结果表明,叶轮和扩压器中的确定应力在数值上相当,通道内的确定应力沿周向分布有较大的梯度、沿流向分布的总体趋势是从交界面向两侧迅速衰减,交界面处的确定应力和其空间相关项之间在数值上存在一定的偏差. Steady and unsteady simulations were conducted in the investigation of deterministic unsteady phenomenon in a transonic centrifugal compressor with splitter blade. Resuits from the steady and unsteady simulations were compared firstly and then the distributions of deterministic stresses in the blade passage and the components of deterministic stresses based on velocity decomposition at the impeller/diffuser interface were studied in depth. The study indicates that the deterministic stresses in the impeller and diffuser are of similar magnitudes, and that the stresses in the passage have large gradients in circumferential direction and decrease rapidly from the interface towards two sides in flow direction, and also shows that the spatial correlations have some discrepancies with the deterministic stresses at the impeller/diffuser interface.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第3期534-540,共7页 Journal of Aerospace Power
基金 国防基础预研项目(A0620060430) 航空支撑科技基金(04B51004)
关键词 航空 航天推进系统 离心压气机 转静干涉 确定应力 数值模拟 aerospace propulsion system centrifugal compressor impeller/diffuser in teraction deterministic stresses numerical simulation
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参考文献11

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二级参考文献10

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共引文献3

同被引文献37

  • 1季路成,温泉,银越千.离心压气机内激波/叶排相互作用[J].工程热物理学报,2006,27(5):766-768. 被引量:1
  • 2赵军,柳阳威,刘宝杰.NASA67级非定常流场的频域分析[J].航空动力学报,2007,22(8):1371-1377. 被引量:12
  • 3张士明,杨策,胡良军,祁明旭,马朝臣.离心压气机内部非定常流场的数值模拟[J].工程热物理学报,2007,28(6):942-944. 被引量:5
  • 4Adamczyk J J.Model equation for simulation flows in multistage turbomachinery[R].ASME Paper 85-GT-226,1985.
  • 5Adamczyk J J.A model for closing the invisid form of the average passage equation system[J].Journal of Turbinemachinery,1986,108(2):180-186.
  • 6Rhie C M,Gleixner A J,Spear D A,et al.Development and application of a multistage Navier-Stokes solver:Part 1 multistage modeling using body-forces and deterministic stresses[R].ASME Paper 95-GT-342,1995.
  • 7Sondak D L,Dorney D J,Davis R L.Modeling turbomachinery unsteadiness with lumped deterministic stresses[R].AIAA 96-2570,1996.
  • 8Van de Wall A J,Kadambi J R,Adamczyk J J.A transport model for the deterministic stresses associated with turbomachinery blade row interaction[J].Journal of Turbomachinery,2000,122(4):593-603.
  • 9Giles M.An approach for multistage calculations incorporating unseadiness[R].ASME Paper 92-GT-282,1992.
  • 10He L,Ning W.Efficient approach for analysis of unsteady viscous flows in turbomachines[J].AIAA Journal,1998,36(11):2005-2012.

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