马宝峰：男，1976年9月出生，教授，博士生导师。
电话：010-82338344 (办)
Email：bf-ma@buaa.edu.cn
办公室：北京航空航天大学新主楼C1115
主要研究方向：
1）飞行器大迎角空气动力学；
2）旋涡分离流的稳定性、演化及其控制研究；
3）飞行器气动外形数值优化研究；
4）高超声速空气动力学、激波边界层干扰
1.教育经历
1996.9—2000.9，北京航空航天大学飞行器设计与应用力学系，飞行器设计与工程专业，工学学士学位
2000.9—2005.6，北京航空航天大学流体力学研究所，流体力学专业，工学博士学位
2.工作经历
2005.6—2007.9，北京航空航天大学航空宇航科学与技术博士后流动站，博士后
2007.9—2009.9，北京航空航天大学流体力学研究所，讲师
2015.5—2016.5，英国巴斯大学机械工程系，访问学者
2009.9—2020.7，北京航空航天大学流体力学研究所，副教授
2020.7—至今，北京航空航天大学流体力学研究所，教授
3.教学
本科生《综合实验》课
研究生《复杂流动引论》课
留学本科生《Experimental Fluid Mechanics》
留学研究生《Introduction to Complex Flow》
4.科研项目
主持国家自然科学基金项目4项、**预研基金、航天基金、航空航天院所合作项目若干项。
5.评审专家
国际期刊Physics of Fluids、AIAA Journal、Journal of Aircraft、Journal of Propulsion and Power、Journal of Visualization、Chinese Journal of Aeronautics等审稿专家；
国家自然科学基金、北京市自然科学基金、航空科学基金等通讯评审专家。
6.所获奖励
中国力学学会 科技进步奖二等奖（马宝峰，邓学蓥），飞行器大迎角复杂空气动力学机理及应用研究, 2019.8.5.
7.发表的主要论文
Hong-Gang Jiang, Bao-Feng Ma, Experiments on self-sustained oscillations of leeward vortices over a hemisphere cylinder, Physics of Fluids, 2019, 31(9):1-16.
Cheng Gong, Bao-Feng Ma, Aerodynamic evaluation of an unmanned aerial vehicle with variable sweep and span, Proc IMechE Part G: J Aerospace Engineering, 2019, 233(13):4980-4997.
Cheng Gong, Bao-Feng Ma, Shape Optimization and Sensitivity Analysis of a Morphing-Wing Aircraft, International Journal of Aeronautical and Space Sciences, 2019, 20:57-69.
Heng Luo, and Bao-Feng Ma, Time-averaged asymmetries and oscillatory global modes of vortex flows over a slender wing, Physics of Fluids, 2018, 30(9), 097101:1-18.
Bao-Feng Ma, and Hong-Gang Jiang, Estimation of perspective errors in 2D2C-PIV measurements for 3D concentrated vortices, Experiments in Fluids, 2018, 59(101): 1-14.
Bao-Feng Ma,and Shuo-Lin Yin, Vortex oscillations around a hemisphere-cylinder body with a high fineness ratio, AIAA Journal, 2018, 56(4): 1402-1420.
Bao-Feng Ma, Zhijin Wang,and Ismet Gursul, Symmetry Breaking and Instabilities of Conical Vortex Pairs over Slender Delta Wings, Journal of Fluid Mechanics, 2017, 832:41-72.
Bao-Feng Ma, Bing Wang, and Xue-Ying Deng, Effects of Reynolds Numbers on Wing Rock Induced by Forebody Vortices, AIAA Journal, 2017, 55(9): 2980-2991.
Ma Baofeng, Deng Xueying, and Wang Bing, Effects of Wing Locations on Wing Rock Induced by Fore-body Vortices, Chinese Journal of Aeronautics, 2016, 29(5): 1226-1236.
Bao-Feng Ma，Yu Huang，and Xue-Ying Deng，Dynamic responses of asymmetric vortices over slender bodies to a rotating tip perturbation, Experiments in Fluids, 2016, 57(4):1-16.
Bao-Feng Ma，Xue-Ying Deng, Zhen Rong，and Bing Wang，The self-excited rolling oscillations induced by fore-body vortices，Aerospace Science and Technology, 2015, 47：299-313.
Bao-Feng Ma, and Tong-Xin Liu, Low-frequency vortex oscillation around slender bodies at high angles-of-attack, Physics of Fluids, 26, 091701, 2014.
Ma Baofeng, Huang Yu, and Liu Tongxin, Low-frequency unsteadiness of vortex wakes over slender bodies at high angle of attack, Chinese Journal of Aeronautics, 27(4), 2014, pp772-780.
Long-Kun Wei, and Bao-Feng Ma, Wing Rock Induced by a Hemisphere-Cylinder Forebody, Journal of Aircraft, Vol.51, No.2, 2014, pp.606-613.
Bing Wang, Xue-Ying Deng, Bao-Feng Ma, Zhen Rong, and Bo-Chao Cao, Modeling of Wing Rock Using Frequency Spectrum Analysis to Free-to-Roll Time History, Journal of Aircraft，2011, 48(3)：805-811.
Bing Wang, Xue-Ying Deng, Bao-Feng Ma, and Zhen Rong, Effects of tip perturbation and wing locations on rolling oscillation induced by forebody vortices，Acta Mechanica Sinica, 2010，26(5)：787-791.
Xueying Deng, Wei Tian, Baofeng Ma, and YanKui Wang, Recent progress on the study of asymmetric vortex flow over slender bodies, Acta Mechanica Sinica, 2008, 24(5)：475-487.
Bao-Feng, Ma, and Xue-Ying, Deng, Tip-Disturbance Effects on Asymmetric Vortex Breakdown of a Chined-Forebody, Journal of Aircraft, Vol.45, No.4, 2008.
Bao-Feng, Ma, Xue-Ying, Deng, and Ying Chen, Effects of Forced Asymmetric Transition on Vortex Asymmetry around Slender Bodies, AIAA Journal, Vol.45, No.11, 2007.
Bao-Feng, Ma, and Xue-Ying, Deng, Vortex Interactions between Chined Forebody and Strake, Journal of Aircraft, Vol.43, No.6, 2006.
Bao-Feng, Ma, Pei-Qing, liu, and Yuan Wei, Effects of Wing and Canard Sweep on Lift Enhancement of Canard Configurations, Journal of Aircraft, Vol.41, No.6, 2004.
