| [1] Rumsey C L, Ying S X. Prediction of high lift: review of present CFD capability[J]. Progress in Aerospace Sciences, 2002, 38(2): 145-180.[2] Zhu Z Q, Chen Y C, Wu Z C. Numerical simulation of high lift system configuration[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(3): 257-262. (in Chinese) 朱自强, 陈迎春, 吴宗成. 高升力系统外形的数值模拟计算[J]. 航空学报, 2005, 26(3): 257-262.[3] Zhang W S, Chen H X, Zhang Y F,et al. Nacelle strake's aerodynamic characteristics effects on high-lift configuration of transport aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(1): 76-85. (in Chinese) 张文升, 陈海昕, 张宇飞, 等. 短舱扰流片对运输机增升装置气动特性的影响[J]. 航空学报, 2013, 34(1): 76-85.[4] Cui Z, Han D, Li J B. Study on aerodynamic characteristics of airfoil with gurney flaps under high subsonic flow[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(10): 2277-2286. (in Chinese) 崔钊, 韩东, 李建波. 翼型加装格尼襟翼的高亚声速气动特性研究[J]. 航空学报, 2013, 34(10): 2277-2286.[5] Rogers S E, Roth K, Nash S M. CFD validation of high-lift flows with significant wind-tunnel effects, AIAA-2000-4218[R]. Reston: AIAA, 2000.[6] van der Burg J W, von Geyr H F, Heinrich R, et al. Geometrical model installation and deformation effects in the European project EUROLIFT II, AIAA-2007-4297[R]. Reston: AIAA, 2007.[7] Heinz H. Overview about the European high lift research programme EUROLIFT, AIAA-2004-0767[R]. Reston: AIAA, 2004.[8] Rudnik R, von Geyr H F. The European high lift project EUROLIFT II-objectives, approach, and structure, AIAA-2007-4296[R]. Reston: AIAA, 2007.[9] Slotnick J P, Hannon J A, Chaffin M. Overview of the first AIAA CFD high lift prediction workshop(invited), AIAA-2011-0862[R]. Reston: AIAA, 2011.[10] Rumsey C L, Long M, Stuever R A. Summary of the first AIAA CFD high lift prediction workshop(invited), AIAA-2011-0939[R]. Reston: AIAA, 2011.[11] Johnson P L, Jones K M, Madson M D. Experimental investigation of a simplified 3D high lift configuration in support of CFD validation, AIAA-2000-4217[R]. Reston: AIAA, 2000.[12] Rogers S E, Roth K, Nash S M. Validation of computed high-lift flows with significant wind-tunnel effect[J]. AIAA Journal, 2001, 39(10): 1884-1892.[13] van Leer B. Towards the ultimate conservative differences scheme[J]. Journal of Computational Physics, 1997, 135: 229-248.[14] Menter F R. Two equation eddy viscosity turbulence models for engineering application[J]. AIAA Journal, 1994, 32(8): 1598-1605.[15] Menter F R, Langtry R B, Likki S R, et al. A correlation based transition model using local variables: part I-model formulation[J]. Journal of Turbomachinery, 2004, 128(3): 413-422.[16] Zhang Y L, Wang G X, Meng D H, et al. Calibration of γ-Reθ transition model[J]. Acta Aerodynamica Sinica, 2011, 29(3): 295-301. (in Chinese) 张玉伦, 王光学, 孟德虹, 等.γ-Reθ转捩模型的标定研究[J]. 空气动力学学报, 2011, 29(3): 295-301.[17] Meng D H, Zhang Y L, Wang G X, et al. Application of γ-Reθ transition model to two-dimensional low speed flows[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(5): 792-801. (in Chinese) 孟德虹, 张玉伦, 王光学, 等. γ-Reθ转捩模型在二维低速问题中的应用[J]. 航空学报, 2011, 32(5): 792-801.[18] Sclafani A J, Slotnick J P, Vassberg J C, et al. Extended OVERFLOW analysis of the NASA trap wing wind tunnel model, AIAA-2012-2919[R]. Reston: AIAA, 2012. |
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