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考虑轴向密流比S1流场仿真技术研究

A Numerical Method for SI Flow Simulation Considering AVDR
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摘要 在二维N-S方程求解器基础上发展了考虑平面叶栅轴向密流比(AVDR)的准三维数值模拟方法,利用DLRV2叶栅实验数据对该求解器进行验证。结果表明:该求解器计算准确性较高,AVDR对叶栅性能及流场影响较大,是不能忽略的因素。本文开发的求解器求解精度较高,收敛速度快,可满足平面叶栅数值仿真要求。 A quasi-three-dimensional solver which considering the AVDR based on the two-dimensional Navier-Stokes(N-S)equations was presented.The solver had been validated through the comparison between the experimental data and numerical simulation results of the subsonic cascade.The results show that the solver can reach a high calculation accuracy which prove that the AVDR is an essential input parameter when the solver simulating a cascade flow flied and performance.The solver has a high accuracy,a fast rate of convergence and could meet the demand of numerical simulation of cascade flow field.
作者 余雅琪 李恩华 唐晓毅 YU Yaqi;LI Enhua;TANG Xiaoyi(AECC Hunan Aviation Powerplant Research Institute,Zhuzhou Hunan 412002;Hunan Key Laboratory of Turbomachinery on Small and Medium Aero-engine,Zhuzhou Hunan 412002)
出处 《中国科技纵横》 2022年第4期70-72,102,共4页 China Science & Technology Overview
关键词 AVDR 平面叶栅 准三维 CFD S1流面 AVDR cascade quasi-three-dimensional CFD Sl stream-face
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  • 1王仲奇,韩万金,黄家骅,黄鸿雁.叶片弦向倾斜对损失发展的影响及叶片反弯降低损失机理的研究[J].工程热物理学报,1996,17(1):25-30. 被引量:2
  • 2王仲奇,工程热物理学报,1990年,11卷,3期
  • 3王正明,工程热物理学报,1986年,7卷,1期
  • 4Wang Z M,Trans ASME J Engineering Gas Turbine Power,1985年,107卷,2期
  • 5Jouini D B M,Sjolander S A,Moustapha S H.Midspan flow-field measurements for two transonic linear turbine cascades at off-design conditions[R].Proceedings of ASME Turbo Expo 2001,New Orleans,USA:2001-GT-0493,2001.
  • 6Saroch M F.Contributions to the study of turbomachincry:Part Ⅱ:Computations of the effects of AVDR on transonic turbine cascades[D].M.Eng.Thesis,Carleton University,Canada:January,1996.
  • 7Kiock R,Lehthaus F,Baines N C,et al.The transonic flow through a plane turbine cascade as measured in four european wind tunnels[J].ASME Journal of Engineering for Gas Turbines and Power,1986,108:277-284.
  • 8Song B,Ng W.Performance and flow characteristics of an optimized supercritical compressor stator cascade[J].ASME Journal of Turbomachinery,2006,128:435-443.
  • 9Song B.Experimental and numerical investigations of optimized high-turning supercritical compressor blades[D].Ph.D.Dissertation,Virginia Polytechnic Institute and State University,2003.
  • 10Song B,Ng W.Influence of axial velocity density ratio in cascade testing of supercritical compressor blades[R].40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit,Fort Lauderdale,Florida:AIAA-2004-3414,2004.

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