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转静干涉对叶片非定常表面压力的影响 被引量：5

Effect of stator-rotor interactions on the blades surface pressure
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摘要 为了研究转静干涉对叶片表面压力的影响,通过数值模拟的方法,计算了一级低速轴流压气机流场,得到了充分收敛的周期性非定常流场解。在此基础上分析了叶片表面压力及气动力的变化规律,并通过改变背压,研究了流量对叶片表面压力和气动力的影响。最后在低速轴流压气机实验器上进行了实验验证,结果表明计算和实验的结果吻合得较好。 To study the stator-rotor interactions on the blades surface pressure,a numerical simulation has been carried out for a low-speed single-stage axial compressor. Results for periodical unsteady flow have been obtained. Based on this,the change law of the pressure and aerodynamic forces on the blades surface has been analyzed. The influence of different mass flow on the pressure and aerodynamic forces on the blades surface has been studied by changing the static pressure of the downstream. Lastly,an experiment has been carried out on the rig of low-speed compressor. The numerical simulation results agree well with the experiment.
作者 王英锋 胡骏 王志强
机构地区 南京航空航天大学能源与动力学院
出处 《推进技术》 EI CAS CSCD 北大核心 2010年第2期198-203,239,共7页 Journal of Propulsion Technology
关键词 压气机 转静干涉 表面压力 气动力 Air compressor Interaction Pressure Aerodynamic force
分类号 V232.4 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献13

  • 1Gorrell S E, Okiishi T H, Copenhaver W W. Stator-rotor inter-actions in a transonic compressor: Part I-effect of blade-row spacing on performance [ J ]. Journal of Turbomachinery, 2003, 125:328 - 335.
  • 2Gorrell S E, Okiishi T H, Copenhaver W W. Stator - rotor inter-actions in a transonic compressor: Part II-description of a loss producing mechanism [ J ]. Journal of Turbomachinery, 2003, 125 : 336 - 345.
  • 3Li H D, He L. Blade count and clocking effects on three- bladerow interaction in a transonic turbine [ J ]. Journal of Turbomachinery, 2003, 125 : 632 - 640.
  • 4Feiereisen J M, Montgomery M D, Fleeter S. Unsteady aerodynamic forcing functions, a comparison between linear theory and experiment [ J ]. Journal of Turbomachinery, 1994, 116:676-685.
  • 5Henderson G, Fleeter S. Forcing function effects on unsteady aerodynamic gust response: Part I - forcing functions [ J]. Journal of Turbomachinery, 1993, 115.
  • 6Hsu S T, Wo A M. Reduction of unsteady blade loading by beneficial use of vortical and potential disturbance in an axial compressor with rotor clocking [ J ]. Journal of Turbomachinery, 1998, 120:705-713.
  • 7Layachi M Y, Bolcs A. Effect of the axial spacing between rotor and stator with regard to the indexing in an axial compressor[ A ]. ASME Proceedings of ASME Turbo Expo ,2001 [ C]. US: Louisiana, 2001.
  • 8邓向阳,张宏武,黄伟光.低速轴流压气机中前后静叶对动叶顶部区域流动的影响[J].航空学报,2005,26(5):535-539. 被引量：13
  • 9周盛,侯安平,弓志强,陆亚钧,葛劲东.关于轴流压气机的非定常两代流型[J].航空学报,2005,26(1):1-7. 被引量：15
  • 10胡骏,汤国才,于再.动叶尾迹对静子非定常气动性能影响的研究[J].航空动力学报,1999,14(4):387-392. 被引量：15

二级参考文献42

  • 1刘景梅,周盛.叶轮机械新流型探索雏议[J].航空动力学报,1995,10(3):205-209. 被引量：6
  • 2周盛,侯安平,弓志强,陆亚钧,葛劲东.关于轴流压气机的非定常两代流型[J].航空学报,2005,26(1):1-7. 被引量：15
  • 3周盛.涡轮风扇发动机气动热力学三项新概念探讨[A]..第176次香山科学会议空天安全的重大基础问题学术讨论会文集[C].北京:中国科学院,2001..
  • 4[1]Rumsey C L. A Comparison of Predictive Capabilities of Several Turbulence Models Using Upwind and Central-Difference Computer Codes. AIAA Paper 93-0192, 1993
  • 5[2]Sturek W B, et al. The Application of CFD to the Prediction of Missile Body Vortices. AIAA Paper 97-0637, 1997
  • 6[3]Swanson R C, Turkel E. On Central-Difference and Upwind Schemes. Journal of Computational Physics, 1992, 101: 292～306
  • 7[4]Baldwin B S, Lomax H. Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows. AIAA Paper 78-257, 1978
  • 8[5]Abid R, Vatsa V N, Johnson D A, Wedan B W. Prediction of Separated Transonic Wing Flows with Nonequilibrium Algebraic Turbulence Model. AIAA Journal, 1990, 28(8): 1426～1431
  • 9[6]Johnson D A. Nonequilibrium Algebraic Turbulence Modeling Considerations for Transonic Airfoils and Wings. AIAA Paper 92-0026, 1992
  • 10[7]Josyula E. Computational Study of High-Angle-of-Attack Missile Flows Using Two-Equation Turbulence Models.AIAA Paper 98-0525, 1998

共引文献77

同被引文献52

  • 1Mailach R, Vogeler K. Aerodynamic blade row interactionin an axial compressor: Part U unsteady profile pressuredistribution and blade forces[J]. Journal of Turbomachin-ery ,2004,126(1) :45-51.
  • 2Mailach R,Muller L,Vogeler K. Rotor-stator interactionsin a four-stage low-speed axial compressor: Part I un-steady profile pressures and the effect of clockingQ]. Jour-nal of Turbomachinery, 2004 ,126(4) : 507-518.
  • 3Mailach R, Muller L, Vogeler K. Rotor-stator interactionsin a four-stage low-speed axial compressor: Part H un-steady aerodynamic forces of rotor and stator blades[J].Journal of Turbomachinery,2004,126(4) :519-526.
  • 4Gorrell S E, Okiishi T H, Copenhaver W W. Stator-rotorinteractions in a transonic compressor: Part I effect ofblade-row spacing on performance [J ]. Journal of Turbo-machinery, 2003 ,125(2):328-335.
  • 5Gorrell S E, Okiishi T H, Copenhaver W W. Stator-rotorinteractions in a transonic compressor Part H : effect ofblade-row spacing on performance [J ]. Journal of Turbo-machinery, 2003 ,125(2):336-345.
  • 6Gorrell S E,Car D,Puterbaugh S L,et al. An investigationof wake-shock in a transonic compressor with DPIV andtime-accurate CFD[R]. ASME Paper GT2005-69107,2005.
  • 7Hsu S T,Wo A M. Reduction of unsteady blade loading bybeneficial use of vertical and potential disturbances in anaxial compressor with rotor clocking[J]. Journal of Turbo-machinery, 1998,120(4):705-713.
  • 8Miller R J, Moss R W, Ainsworth R W? et al. Wake,shock,and potential field interactions in a 1. 5 stage tur-bine :Part I vane-rotor and rotor-vane interaction [J].Journal of Turbomachinery, 2003,125(1) : 33-39.
  • 9ZHAO Ben, YANG Ce, HU Liangjun, et al. Investigationof separating and utilizing the influences of up and downstream blade rows[R]. ASME Paper GT2012-68371,2012.
  • 10He N, Tourlidakis A,Elder R L. Comparisons of steadyand time-averaged unsteady flow predictions for impeller-diffuser interactions in a centrifugal compressor stage[R].ASME Paper GT2007-27985 ,2007.

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