Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row

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PDF(370 KB)
Frontiers in Energy ›› 2008, Vol. 2 ›› Issue (3) : 320-325. DOI: 10.1007/s11708-008-0041-2

Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row

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Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row

  • JIANG Jian1, LIU Bo2, WANG Yangang2, NAN Xiangyi2
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Abstract

Numerical simulation of three-dimensional turbulent flow in a multistage axial compressor blade row is conducted. A high resolution, third-order ENN scheme is adopted to catch the shockwave and simulate the turbulent flow correctly,

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. Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row. Frontiers in Energy. 2008, 2(3): 320-325 https://doi.org/10.1007/s11708-008-0041-2

参考文献

1. Yao Jixian, Liu Qianzhi, Zhou Xinhai . Numerical analysis of three-dimensional turbulent flowin compressor blade row by implicit high-resolution scheme. Journal of Aerospace Power, 1996, 11(3): 225–228 (in Chinese)
2. Wang Yangang . Research on mixing process in trailing edge ejection for a tubineblade. Dissertation for the Doctoral Degree. Xi'an: NorthwesternPolytechnical University, 2005, 14–17 (in Chinese)
3. Zhan Hanxin, Shen Mengyu . Computaional Fluid Dynamics-Fundamentalsand Applications of Finite Difference Methods. Beijing: Publishing Company ofNational Defence Industry, 2003, 184–191 (in Chinese)
4. Zhan Hanxin, He Guohong, Zhang Lei . Some Important Problems for High Order Accurate DifferenceScheme Solving Gas Dynamic Equations. ACTAaerodynamic sinica, 1993, 11(4): 347–356 (in Chinese)
5. Yoon S, Jameson A . Lower-upper symmetric-gauss-seidelmethod for the Euler and Naiver-Stokes equations. AIAA Journal, 1988, 26(9): 1025–1026. doi:10.2514/3.10007
6. Jeong Y, Choi S O . Memory optimization of LU-SGScode for the acceleration on latest microprocessors. AIAA Paper 2003-0443, 2003
7. Wang Baoguo, Huang Hongbin . Calculation Method for Flowfieldof Transonic and Subsonic Turbomachinery. Beijing: Publishing Company ofNational Defence Industry, 2000, 130–131 (in Chinese)
8. Wu Xianhong, Chen Maozhang . Two –Dimensional NumericalSimulation of Unsteady Rotor/Stator Interaction. Journal of Aerospace Power, 1998, 13(2): 128–132 (in Chinese)
9. Denton J D . The calculation of three dimensional viscous flow through multistageturbomachines. ASME Journal Turbomachinery, 1992, 114(1): 18–26. doi:10.1115/1.2927983
10. Wang L X, Caughey D A . Multiblock/Multigrid EulerMethod to Simulate 2D and 3D Compressible Flow. AIAA Paper 1993-0332, 1993
11. Shyy W, Liu J, Wright J . Pressure-based viscous flow computation using multiblockoverlapped curvilinear grids. NumericalHeat Transfer, Part B, 1994, 25: 39–59. doi:10.1080/10407799408955909
12. Yao Zheng . The analysis of interrow mixing treatment in the calculation of 3Dflow in multistage turbomachinery. Journalof Engineering Thermophysics, 1996, 17(4): 417–422 (in Chinese)
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