[1] Roberts W B. Axial Compressor Performance Restoration by Blade Profile Control[R]. ASME 84-GT-232.
[2] Garzon V E, Darmofal D L. Impact of Geometric Variability on Axial Compressor Performance[R]. ASME GT 2003-38130.
[3] Kumar A, Keane A J, Nair P B, et al. Robust Design of Compressor Blades Against Manufacturing Variations[R]. ASME DETC 2006-99304.
[4] Dow E A, Wang Q. Simultaneous Robust Design and Tolerancing of Compressor Blades[R]. ASME GT 2014-25795.
[5] Chen H, Wang Q, Hu R, et al. Conditional Sampling and Experiment Design for Quantifying Manufacturing Error of Transonic Airfoil[R]. AIAA 2011-658.
[6] 罗华玲, 乔渭阳, 许开富. 大负荷低压涡轮叶型分离转捩流动的大涡模拟[J]. 推进技术, 2009, 30(4). (LUO Hua-ling, QIAO Wei-yang, XU Kai-fu. Large Eddy Simulation of Separated Flow Transition on a Highly-Loaded Low Pressure Turbine Profile[J]. Journal of Propulsion Technology, 2009, 30(4).)
[7] Wang L. Karhunen-Loeve Expansions and Their Applications[D]. UK: London School of Economics and Political Science, 2008.
[8] Berlinet A, Thomas-Agnan C. Reproducing Kernel Hilbert Spaces in Probability and Statistics[M]. Berlin: Springer Science & Business Media, 2011.
[9] Wiener N. The Homogeneous Chaos[J]. American Journal of Mathematics, 1938, 60(4): 897-936.
[10] Xiu D, Karniadakis G E. Modeling Uncertainty in Flow Simulations via Generalized Polynomial Chaos[J]. Journal of Computational Physics, 2003, 187(1): 137-167.
[11] Bungartz H J, Griebel M. Sparse Grids[J]. Acta Numerica, 2004, 13: 147-269.
[12] Daum F, Huang J. Curse of Dimensionality and Particle Filters[C]. Montana: Aerospace Conference, 2003.
[13] Gerstner T, Griebel M. Numerical Integration Using Sparse Grids[J]. Numerical Algorithms, 1998, 18(3-4): 209-232.
[14] Lake J P, King P I, Rivir R B. Reduction of Separation Losses no a Turbine Blade with low Reynolds Number[R]. AIAA 99-0242.
[15] 孙爽, 雷志军, 朱俊强, 等. 粗糙度对超高负荷低压涡轮边界层影响[J]. 推进技术, 2014, 35(3): 347-355. (SUN Shuang, LEI Zhi-jun, ZHU Jun-qiang, et al. Effects of Roughness on Boundary Layer of Ultra-High-Lift Low-Pressure Turbine[J]. Journal of Propulsion Technology, 2014, 35(3): 347-355.)
[16] Zhou C, Hodson H, Himmel C. The Effects of Trailing Edge Thickness on the Losses of Ultrahigh Lift Low Pressure Turbine Blades[J]. Journal of Turbomachinery, 2014, 136(8).
[17] Schlichting H, Gersten K. Boundary-Layer Theory[M].Berlin: Springer Science & Business Media, 2003.
[18] Greitzer E M, Tan C S, Graf M B. Internal Flow: Concepts and Applications[M]. UK: Cambridge University Press, 2007. 收稿日期:2016-05-13;修订日期:2016-06-08。作者简介:颜勇,男,硕士生,研究领域为叶轮机械不确定性分析。E-mail: yy12324@163.com(编辑:史亚红)
|