馬寶峰(北京航空航天大學副教授)

男，生於遼寧省大石橋市，現為北京航空航天大學副教授、研究生導師。

基本介紹

• 中文名：馬寶峰
• 國籍：中國
• 出生地：遼寧省大石橋市
• 職業：副教授
• 畢業院校：北京航空航天大學

教育經歷

2000年本科畢業於北京航空航天大學飛行器設計與工程專業，並被免試推薦為碩博連讀研究生；
2005年於北京航空航天大學獲流體力學專業博士學位；

工作經歷

2005.6—2007.9，北京航空航天大學航空宇航科學與技術博士後流動站，博士後
2007.9—2009.9，北京航空航天大學流體力學研究所，講師
2015.5—2016.5，英國巴斯大學機械工程系，訪問學者
2009.9—至今，北京航空航天大學流體力學研究所，副教授

教學工作

本科生《綜合實驗》課、本科生《科研訓練》、本科生導師、班主任
研究生課《複雜流動引論》；
留學生課《Introduction to Complex Flow》。

目前主要研究興趣

1）飛行器大迎角空氣動力學；
2）飛行器旋渦分離流的穩定性、演化及其控制研究；
3）飛行器氣動外形數值最佳化研究；
4）飛行器超聲速/高超聲速飛行時的音爆、激波邊界層干擾
研究方法：以理論分析和數值模擬為主、結合部分實驗研究

發表的主要論文

1. Bao-Feng Ma, Shuo-Lin Yin, Vortex oscillations around a hemisphere-cylinder body with a high fineness ratio, AIAA Journal, 2018 (online).
2. Bao-Feng Ma, Zhijin Wang, Ismet Gursul, Symmetry Breaking and Instabilities of Conical Vortex Pairs over Slender Delta Wings, Journal of Fluid Mechanics, 2017, 832:41-72.
3. 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.
4. 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.
5. 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.
6. 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.
7. 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.
8. 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.
9. 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.
10. 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.
11. 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.
12. 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.
13. 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.
14. 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.
15. Bao-Feng, Ma, and Xue-Ying, Deng, Vortex Interactions between Chined Forebody and Strake, Journal of Aircraft, Vol.43, No.6, 2006.
16. 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.