Investigation of separation mechanism for airfoil leading edge flow at low Reynolds number

[1] Muti Lin J C, Pauley L L. Low-Reynolds-number separation on an airfoil . AIAA J, 1996, 34(8):1570~1577 [2] Lissaman P B S. Low-Reynolds-number airfoils[J]. Ann Rev Fluid Mech, 1983, 15:223~239 [3] Dovgal A V, Kozlov V V, Michalke A. Laminar boundary layer separation:instability and associated phenomena[J]. Prog Aerospace Sci, 1994, 30:61~94 [4] Mueller T J, Batill S M. Experimental studies of separation on a two-dimensional airfoil at low Reynolds numbers[J]. AIAA J, 1982, 20(4):457~463 [5] Liebeck R H. Laminar separation bubbles and airfoil design at low Reynolds numbers . AIAA 92-2735, 1992 [6] Pauley L L, Moin P, Reynolds W C. The structure of two-dimensional separation[J]. J Fluid Mech, 1990, 220:397~411 [7] Alam M, Sandham N D. Direct numerical simulation of ‘short’ laminar separation bubbles with turbulent reattachment[J]. J Fluid Mech, 2000, 403:223~250 [8] 叶 建, 林国华, 邹正平, 等. 低雷诺数下二维翼型绕流的流场特性分析 . 航空动力学报, 2003, 18(1):38~45 Ye Jian, Lin Guohua, Zou Zhengping, et al. The analysis of flow around a 2-D airfoil at low Reynolds number[J]. Journal of Aerospace Power, 2003, 18(1):38~45(in Chinese) [9] 陆宏志. 叶轮机叶片前缘流动和前缘形状优化 . 北京:北京航空航天大学能源与动力工程学院,2003 Lu Hongzhi. Flow around the leading edge of turbomachinery blading and improved design for leading edge shapes . Beijing:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, 2003(in Chinese)