孟宣市


的个人主页 http://jszy.nwpu.edu.cn/mengxuanshi

  被浏览次数:4661

基本信息 The basic information

孟宣市

航空学院

博士研究生毕业

博士

副教授

力学

mxsbear@nwpu.edu.cn

工作经历 Work Experience

1996-2000,西北工业大学飞机系,空气动力学及飞行力学专业,学士学位

2002-2005,西北工业大学航空学院流体系,流体力学专业,硕士学位

2004-2008,西北工业大学航空学院流体系,流体力学专业,博士学位

2008-,西北工业大学航空学院讲师(2008)、副教授(2011)

2016-2017,美国迈阿密大学(University of Miami),访问学者

教育教学 Education And Teaching

1、《线性代数》,本科生课程, 40学时

2、《实验空气动力学》,本科生课程, 40学时

3、《Experimental Fluid Dynamics》,本科生课程(留学生),24学时

4、《Advanced Measurement and Visualization Techniques in Aerodynamics》,本科生课程(留学生),24学时

5、《现代流动控制基础及应用》,研究生课程,20学时

6、获航空学院 20102011年度本科生教学 最满意青年教师

7、参与西北工业大学“全英语教学课程”立项建设2项。《 Experimental  Dynamics Fluid 》、《Aerodynamics


招生信息 Admission Information

招生研究方向

1、三角翼分离涡的稳定性研究

2、等离子体气动激励特性及机理研究

3、大迎角下细长前体分离涡的稳定性研究及其控制

4、低雷诺数下等离子体对翼型层流分离的主动流动控制 

5、等离子体激励在飞机防/除冰上的应用

科学研究 Scientific Research

[1] 《等离子体激励对低雷诺数下翼型层流分离特性的影响及机理研究》, 国家自然基金,2017/01 – 2020/12,总经费68万。

[2] 《不同时间尺度NS-DBD热效应及流动控制机理研究》, 国家自然基金(参与),2018/01 – 2021/12,总经费62万。

[3] 《脉冲协同射流翼型高升阻比效应及其湍流掺混机理研究》, 国家自然基金(参与),2017/01 – 2020/12,总经费72万。

[4] 《翼型前缘等离子体激励防冰技术及其机理研究》, 国家级重点实验室基金,2017/01 – 2019/12,总经费40万。

[5] 《等离子体激励对飞行器纵向气动力特性的影响及机理研究》,国家自然基金,2011/01 – 2014/12,总经费26万。

[6] 《等离子体激励对低雷诺数下层流分离气泡的影响研究》,国家级重点实验室基金,2014/01 - 2015/12,总经费25万。

[7] 《纳秒脉冲等离子体防除冰机理研究》,西北工业大学基础研究基金,2014/01 - 2016/12,总经费15万。

[8] 《细长体非对称涡等离子体控制机理研究》,高等学校博士点专项科研基金(教育部科技发中心),2010/01 - 2012/12,总经费3.6万。

[9] 《飞行器细长前体涡流场等离子体主动控制机理研究》,中国博士后基金(中国博士后科学基金会),2010/05 - 2011/09,总经费3.0万。

学术成果 Academic Achievements

教材编写:


高永卫,孟宣市,肖春生. 《实验流体力学基础》第2版,西北工业大学出版社,2011年,西安。


代表性文献:

2018年

[1] Xuanshi Meng, Haiyang Hu, Xu Yan, Feng Liu and Shijun Luo. Lift improvements using duty-cycled plasma actuation at low Reynolds numbers, Aerospace Science and Technology, Junuary 2018, 72: 123-133.

[2] Xuanshi Meng, Yuexiao Long, Jianlei Wang, Feng Liu, and Shijun Luo. Dynamics and control of the vortex flow behind a slender conical forebody by a pair of plasma actuators, Physics of Fluids, 2018, 30(2): 024101.

[3] Afaq Ahmed Abbasi, Huaxing Li, Xuanshi Meng, Shiqing Yin, Yuqi Qin, Haiyang Hu, Effect of plasma leading edge tubercles on wing performance, AIAA paper 2018-0679 (2018).

[4] Yuexiao Long, Huaxing Li, Xuanshi Meng, Haiyang Hu, Optimized plasma actuation on asymmetric vortex over a slender body, Applied Physics Letters, 2018, 112(1):014101. 


2017 年

[1] Jinsheng Cai, Yongqiang Tian, Xuanshi Meng, Xuzhao Han, Duo Zhang, Haiyang Hu. An experimental study of icing control using DBD plasma actuator. Experiments in Fluids, August 2017, 58:102.


2016

[1] Xuanshi Meng, Zhide Qiao, Chao Gao, Feng Liu, and Shijun Luo. Effect of Dorsal Fin on Symmetry of Vortices over Slender Delta Wing [J]. AIAA Journal, 54( 8) : 2277-2284, 2016. (SCI)

[2] Yuexiao Long, Huaxing Li, Xuanshi Meng, Feng Liu, and Shijun Luo. Influence of Actuating Position on Asymmetric Vortex Control with Nanosecond Pulse DBD Plasma Actuators. IEEE Transactions on Plasma Science, 2016: 1-11. (SCI)

[3] 孟宣市杨泽人,陈琦,白鹏,胡海洋.  低雷诺数下层流分离的等离子体控制[J]. 航空学报. 37(7): 2112-2122, 2016. (EI)

[4] Xuanshi Meng, Jinsheng Cai, Yongqiang Tian, Xuzhao Han, Duo Zhang, Haiyang Hu. Experimental Study of Deicing and Anti-icing on a Cylinder by DBD Plasma Actuation. 2016, AIAA Paper 2016-4019.(EI)

[5] Liu Yang, Xuanshi Meng, Xu Yan, Feng Liu and Shijun Luo. Experimental and Numerical Study of Laminar Separation on Elliptic Airfoil at Low Reynolds Numbers. 2016, AIAA Paper 2016-4342.(EI)

[6] Haiyang Hu, Huaxing Li, Xuanshi Meng, Xu Yan, Feng Liu, Shijun Luo. Optimization of Dielectric Barrier Discharge Plasma Actuators for Conical-Forebody Flow Control. 2016, AIAA Paper 2016-4018.(EI)

[7] Xu Yan, Huaxing Li, Xuanshi Meng, Liu Yang, Feng Liu, and Shijun Luo. Separation Control Using Plasma Actuator on an Elliptic Airfoil at Low Reynolds Numbers. 2016, AIAA Paper 2016-3622.(EI)

[8] Li Mingyang, Meng Xuanshi, Li Huaxing, Liu Feng, Luo Shijun. Laminar Separation Bubbles Flow Control over Airfoil Using SDBD Plasma Actuator, 2016, AIAA Paper 2016-0842.(EI)

[9] Zhao Jinan, Meng Xuanshi, Wang Jianlei, Liu Feng, and Luo Shijun. Pressure Characteristics over 20 deg Cone Forebody at Alpha 35 deg and Re = (0.1-0.9) × 106[C], 2016, AIAA paper 2016-0592.(EI)

[10] Yuexiao Long, Huaxing Li, Xuanshi Meng, Haiyang Hu, Feng Liu, Shijun Luo. Conical Forebody Flow Control Using Thick Dielectric Barrier Plasma Actuators. 2016, AIAA Paper 2016-0057.(EI)

2015

[1] Meng Xuanshi, Yan Xu, Hu Haiyang, Liu Feng, and Luo Shijun. Plasma Laminar Separation Bubble Control over Airfoil at Low Reynolds Numbers, 2015, AIAA Paper 2015-2954.(EI)

[2] Han Xuzhao, Li Huaxing, Meng Xuanshi, Liu Feng, and Luo Shijun. Effect of Voltage and Frequency on Starting Repetitive Nanosecond Pulsed DBD[C], 2015, AIAA paper 2015-2810. (EI)

[3] Haiyang Hu, Huaxing Li, Xuanshi Meng, Jianlei Wang, Feng Liu, Shijun Luo. Starting Flow by Repetitive Nanosecond Pulsed DBD Actuation at Microseconds and Milliseconds in Quiescent Air. 2015, AIAA Paper 2015-2956.

[4] Zhang Duo, Meng Xuanshi, Wang Jianlei, Liu Feng, and Luo Shijun. Pressures over a Conical Forebody under Repetitive Nanosecond Pulse SDBD Actuations[C], 2015, AIAA Paper 2015-2955.(EI)

[5] Wang Jianlei, Li Huaxing, Meng Xuanshi, Zhang Duo, Liu Feng, and Luo Shijun. Nanosecond SDBD Actuation over a Conical Forebody at Wind Speed 72 m/s and Angle of Attack 45 degree[C], 2015, AIAA Paper 2015-3310. (EI)

2014

[1] Yang Zeren, Meng Xuanshi, Li Wenfeng, Cai Jinsheng. Vortex Flow Control over a Delta Wing Using Leading-edge Rudder. 2014, AIAA Paper 2014-0956. (EI)

[2] Chen Qi, Meng Xuanshi, Wang Yushuai, Luo Shijun and Liu Feng. Comparison of Pressures Driven by Nanosecond Pulses to AC Results[C]. 2014, AIAA Paper 2014-0094. (EI)

[3] Long Yuexiao, Li Huaxing, Meng Xuanshi, Shijun Luo and Feng Liu. Flow Control over a Conical Forebody Using Pulsed Nanosecond Discharge Actuators [C]. 2014, AIAA Paper 2014-0933. (EI)

[4] 李结, 李华星, 王健磊, 孟宣市. 纳秒脉冲等离子体对静止大气的激励特性,西北工业大学学报, 32(2): 176-180, 2014. (EI)

2013

[1] 孟宣市,王健磊,蔡晋生,刘锋,罗时钧. 不同形式等离子体激励对细长体分离涡的控制[J]. 空气动力学学报, 31(5): 647-651+669, 2013.

[2] Meng Xuanshi, Wang Yushuai, Wang Jianlei, Luo Shijun, Liu Feng. Body Force Produced by Plasma Actuator Using PIV and Pressure Measurements. 2013, AIAA Paper 2013-0396. (EI)

[3] Meng Xuanshi, Wang Jianlei, Cai Jinsheng, Luo Shijun, Liu Feng. Optimal DBD Duty Cycle for Conical Forebody Side-Force Proportional Control. 2013, AIAA Paper 2013-0347. ( EI)

2012

[1] 孟宣市, 蔡晋生, 罗时钧, 刘锋. 低背鳍对细长平板三角翼分离涡稳定性影响的研究[J]. 实验流体力学, 26(3): 45-49, 2012. (EI)

[2] Meng Xuanshi, Wang Jianlei, Cai Jinsheng, Luo Shijun, Liu Feng. Effect of plasma actuation on asymmetric vortex flow over a conical forebody. 2012, AIAA Paper 2012-0787. (EI)

[3] Tian Bin, Li Huaxing, Meng Xuanshi, Liu Feng, Luo Shijun. Flow control over conical forebody with port pulsed plasma actuator [C]. 2012, AIAA Paper 2012-0289. (EI)

2011

[1] Meng Xuanshi, Cai Jinsheng, Qiao Zhide, Luo Shijun, Liu Feng. Experimental Investigations on Stability of Vortex Flow over Slender Delta Wing with Dorsal Fin[C]. 2011, AIAA Paper 2011-486.

[2] Meng Xuanshi, Cai Jinsheng, Qiao Zhide, Luo Shijun, Liu Feng. Unsteady Plasma Flow Control over Conical Forebody. Proceeding of the Sixth International Conference on Fluid Mechanics, June 30-July 3, 2011, Guangzhou, China. (ISI: 000288362800050)

2010

[1] Meng Xuanshi, Qiao Zhide, Gao Chao, Luo Shijun, Liu Feng. Effect of Dorsal Fin on the Stability of Vortices over a Delta Wing[J]. Modern Physics Letters B, 24(13): 1389-1392. May, 2010. (SCI)

[2] Meng Xuanshi, Guo Zhixi, Luo Shijun, Liu Feng. Ensemble and Phase-Locked Averaged Loads Controlled by Plasma Duty Cycles[C]. 2010, AIAA Paper 2010-878. (EI)

[3] Meng Xuanshi, Guo Zhixi, Luo Shijun, Liu Feng. Ensemble and Phase-Locked Averaged Loads Controlled by Plasma Duty Cycles[C]. AIAA Paper 2010-878, 2010. (EI)

[4] 孟宣市, 郭志鑫, 刘锋, 罗时钧. 细长圆锥前体非对称涡流场的等离子体控制[J]. 航空学报. 31(3): 500-505, 2010.EI

2009

[1] 孟宣市, 乔志德, 高超,罗时钧,刘锋. 低背鳍对细长平板三角翼流场影响的PIV测量[J].  航空学报, 2009, 30(12): 2295-2300. (EI) 

[2] 孟宣市,乔志德, 高超,罗时钧,刘锋. 带背鳍平板三角翼分离涡显示与测量[J].  空气动力学学报, 2009, 27(6): 645-649. (EI)

[3] 孟宣市,贾春,乔志德, 高超,罗时钧,刘锋. 20度圆锥在低速35度迎角下的压力分布特性[J]. 西北工业大学学报, 2009, 27(2): 145-150. (EI)



















综合介绍 General Introduction

多次前往美国、欧洲等国家和地区进行合作交流,并在美国迈阿密大学访学一年、加州大学尔湾分校进行过短期学习,与迈加州大学尔湾分校机械宇航系(Dept. of Mechanical and Aerospace Engineering, University of California, Irvine)、阿密大学机械宇航系( Dept. of Mechanical and Aerospace Engineering, University of Miami)、爱荷华州立大学机械宇航系(Dept. of Aerospace Engineering, Iowa State University)、新加坡国立大学淡马锡研究所(Temasek Laboratories, National University of Singapore) 等高校与研究所保持着密切的合作交流。西北工业大学2011年度翱翔之星,先后主持国家自然基金、航空基金,教育部博士点基金、中博士后基金、总装备部重点实验室基金、西工大基础研究基金以及院所横向课题等项目,并参与国家“863”、“973”、自然科学基金等多项科研项目。