[1] Smith L H, Jr. The radial-equilibrium equation of turbomachinery[J]. Journal of Engineering for Power, 1966, 88(1): 1-12.
[2] Jin H L, Jin D H, Li X J, et al. A time-marching throughflow model and its application in transonic axial compressor[J]. Journal of Thermal Science, 2010, 19(6): 519-525.
[3] Horlock J H, Denton J D. A review of some early design practice using computational fluid dynamics and a current perspective[J]. Transactions of the ASME Journal of Turbomachinery, 2005, 127(1): 5-13.
[4] Denton J D, Dawes W N. Computational fluid dynamics for turbomachinery design[J]. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 1999, 213(2): 107-124.
[5] Spurr A. The prediction of 3D transonic flow in turbomachinery using a combined throughflow and blade-to-blade time marching method[J]. International Journal of Heat Fluid Flow, 1980, 2(4): 189-199.
[6] Baralon S, Erikson L E, Hall U. Validation of a throughflow time-marching finite-volume solver for transonic compressors, ASME Paper, 1998-GT-47[R]. 1998.
[7] Li X J, Jin H L, Gui X M. Performance numerical investigation of double-channel fan/compressor[J]. Journal of Aerospace Power, 2009, 24(12): 2719-2726. (in Chinese) 李晓娟, 金海良, 桂幸民. 风扇/增压级内外涵联算的特性数值模拟[J]. 航空动力学报, 2009, 24(12): 2719-2726.
[8] Simon J F, Leonard O. Modeling of 3-D losses and deviations in a throughflow analysis tool[J]. Journal of Thermal Science, 2007, 16(3): 1-7.
[9] Jin H L. Application of circumferentional average method in multistage axial fan/compressor design and analysis[D]. Beijing: School of Energy and Power Engineering, Beihang University, 2011. (in Chinese) 金海良. 周向平均方法在多级轴流风扇/压气机设计与分析中的应用[D]. 北京: 北京航空航天大学能源与动力工程学院, 2011.
[10] Wan K, Jin H L, Jin D H, et al. Influence of non-axisymmetric terms on circumferentially averaged method in fan/compressor[J]. Journal of Thermal Science, 2013, 22(1): 13-22.
[11] Zhu F, Jin D H, Gui X M. Corner flow control in high through-flow axial commercial fan/booster using blade 3-D optimization[J]. Journal of Thermal Science, 2012, 21(1): 32-41.
[12] Baralon S, Erikson L E, Hall U. Evaluation of high-order terms in the throughflow approximation using 3D Navier-Stokes computations of a transonic compressor rotor. ASME Paper[R], 1999-GT-74, 1999.
[13] Simon J F. Contribution to throughflow modelling for axial flow turbomachines[D]. Liège: Faculty of Applied Science, University of Liège, 2007.
[14] Ning F F. Numerical investigations of flows in transonic compressors with real geometrical complexities[D]. Beijing: School of Energy and Power Engineering, Beihang University, 2002. (in Chinese) 宁方飞. 考虑真实几何复杂性的压气机内部流动的数值模拟[D]. 北京: 北京航空航天大学能源与动力工程学院, 2002.
[15] Gentry R A, Martin R E, Daly B J. An Eulerian differencing method for unsteady compressible flow problems[J]. Journal of Computational Physics, 1966, 1(1): 87-118.
[16] Bosman C, Marsh H. An improved method for calculating the flow in turbo-machines, including a consistent loss model[J]. Journal of Mechanical Engineering Science, 1974, 16(1): 25-31.
[17] Edwards J R. A low-diffusion flux-splitting scheme for Navier-Stokes calculations[J]. Computers and Fluids, 1997, 26(6): 635-659.
[18] Frost G R, Wennerstrom A J. The design of axial compressor airfoils using arbitrary camber lines, ARL-73-0107 (AD 765165)[R]. 1973.
[19] Ji G F, Gui X M. A blading design method for axial/centrifugal compressor airfoils using arbitrary camber lines[J]. Journal of Aerospace Power, 2009, 24(1): 150-156. (in Chinese) 冀国锋, 桂幸民. 轴流/离心压气机通用任意中弧造型设计方法研究[J]. 航空动力学报, 2009, 24(1): 150-156. |