[1] 牟让科, 杨永年. 飞机抖振问题研究进展[J]. 应用力学学报, 2001, 18(增刊): 142-150. Mou Rangke, Yang Yongnian. Advances of studies for the buffet problem of aircraft [J]. Chinese Journal of Applied Mechanics, 2001, 18(SI): 142-150. (in Chinese)
[2] 罗建国, 张建柏. 机翼抖振边界的N-S方程预测//第七届空气弹性学术交流会文集, 2001: 67-73. Luo Jianguo, Zhang Jianbai. Buffet boundary prediction of wing with Navier-Stokes equations//The Seventh Academic Exchange Congress of Aeroelastisity Press. 2001: 67-73. (in Chinese)
[3] 牟让科, 杨永年, 叶正寅. 超临界翼型的跨音速抖振特性[J]. 计算物理, 2001, 18(5): 477-480. Mou Rangke, Yang Yongnian, Ye Zhengying. Buffet characteristics of supercritical airfoil at transonic flow[J]. Chinese Journal of Computational Physics, 2001, 18(5): 477-480. (in Chinese)
[4] Mitchell D J. Introduction to transonic aerodynamics of airfoils and wings [M]. London: Engineering Science Data Unit, 1990: 1-46.
[5] David N. Transonic aerodynamics [M]. New York: American Institute of Aeronautics and Astronautics, 1981: 81-145.
[6] Charles D H. NASA supercritical airfoils. NASA Technical Paper 2969, 1990.
[7] 程不时, 李云军, 王智宇,等. 飞机设计手册-民用飞机总体设计[M]. 北京: 航空工业出版社, 2005. Cheng Bushi, Li Yunjun, Wang Zhiyu, et al. Aircraft design handbook-commercial aircraft general design[M]. Beijing: Aviation Industry Press, 2005. (in Chinese)
[8] MilholenII W E, Owens L R. On the application of contour bumps for transonic drag reduction. AIAA-2005-426, 2005.
[9] Ogawa H, Babinsky H. Evaluation of wave drag reduction by flow control. AIAA-2005-1415, 2005.
[10] Caruana D, Correge M, Reberga O, et al. Buffet and buffeting active control . AIAA-2000-2609, 2000.
[11] Cook P H, McDonald M A, Firmin M C P. Aerofoil RAE2822 pressure distributions, and boundary layer and wake measurements. AGARD-AR-138, A6, 1979.
[12] 董璐. 飞机抖振特性N-S方程计算. 南京: 南京航空航天大学航空宇航学院, 2007. Dong Lu. Numerical studies of aircraft buffet with Navier-Stokes equations . Nanjing: College of Aerospace En-gineering, Nanjing University of Aeronautics and Astronautics, 2007. (in Chinese)
[13] 道格拉斯飞机公司来华技术座谈气动小组资料汇编. 第三机械工业部第六二八研究所, 1979. Douglas Aircraft Company aerodynamics group technology discussion compiled. The 628 Institute of the Third Machinery Industry, 1979. (in Chinese)
[14] Chung I J, Lee D J, Reu T K. Prediction of transonic buffet onset for an airfoil with shock induced separation bubble using steady Navier-Stokes solver . AIAA-2002-2934, 2002.
[15] Wu H Y, Yang S C, Liu F. Comparison of three geometric representations of airfoils for aerodynamic optimization. AIAA-2003-4095, 2003. |