联系方式
常军涛 教授
传真 **
邮箱 changjuntao@hit.edu.cn
邮编 150001
通信地址 哈尔滨市南岗区一匡街2号哈工大科学园知源楼3047信箱
教育与工作经历
1998年9月-2002年7月哈尔滨工业大学 热能与动力工程专业本科， 获本科学位
2002年9月-2007年11月哈尔滨工业大学 动力机械与工程专业硕博， 获博士学位
2008年3月-2010年12月哈尔滨工业大学 基础与交叉科学研究院， 讲师
2011年1月-2015年12月哈尔滨工业大学 基础与交叉科学研究院， 副教授
2013年04月-至今哈尔滨工业大学 能源科学与工程学院， 博士生导师
2016年01月-至今哈尔滨工业大学 基础与交叉科学研究院， 入选“青年拔尖教授”计划
基本信息
常军涛，男，汉族，1981年生。教授职称，博士生导师。目前在哈尔滨工业大学基础与交叉科学研究院 高超声速技术研究中心工作。
2007年11月哈工大博士毕业，2008年1月开始在哈工大控制科学与工程从事博士后研究工作，2008年3月在哈尔滨工业大学留校任教，2010年12月破格评为副教授，2011年12月博士后出站，2013年4月评为博士生导师， 2016年1月入选哈尔滨工业大学“青年拔尖教授”计划。
近几年先后主持中国博士后基金面上项目、中国博士后基金特别资助项目、国家自然科学青年基金项目、国家自然科学面上基金项目、航天科工集团横向课题、总装备部重大专项项目等10余项。在高超声速进气道不起动机理、状态监测、控制等方面共计发表论文80余篇，其中SCI检索60余篇。申报中国发明专利及国防发明专利20项，其中已授权15项。
主要学术任职
下列杂志的特约审稿人：
国内：《航空学报》、《航空动力学报》、《推进技术》、《固体火箭技术》；
国外：《Acta Astronautica》、《Journal of Propulsion and Power》、《ASCE's Journal of Aerospace Engineering》、《Aerospace Science and Technology》
国家自然基金评议专家
-----------------------------------------------------------------
基本信息
联系方式
常军涛 教授
传真 **
邮箱 changjuntao@hit.edu.cn
邮编 150001
通信地址 哈尔滨市南岗区一匡街2号哈工大科学园知源楼3047信箱
教育与工作经历
1998年9月-2002年7月哈尔滨工业大学 热能与动力工程专业本科， 获本科学位
2002年9月-2007年11月哈尔滨工业大学 动力机械与工程专业硕博， 获博士学位
2008年3月-2010年12月哈尔滨工业大学 基础与交叉科学研究院， 讲师
2011年1月-2015年12月哈尔滨工业大学 基础与交叉科学研究院， 副教授
2013年04月-至今哈尔滨工业大学 能源科学与工程学院， 博士生导师
2016年01月-至今哈尔滨工业大学 基础与交叉科学研究院， 入选“青年拔尖教授”计划
基本信息
常军涛，男，汉族，1981年生。教授职称，博士生导师。目前在哈尔滨工业大学基础与交叉科学研究院 高超声速技术研究中心工作。
2007年11月哈工大博士毕业，2008年1月开始在哈工大控制科学与工程从事博士后研究工作，2008年3月在哈尔滨工业大学留校任教，2010年12月破格评为副教授，2011年12月博士后出站，2013年4月评为博士生导师， 2016年1月入选哈尔滨工业大学“青年拔尖教授”计划。
近几年先后主持中国博士后基金面上项目、中国博士后基金特别资助项目、国家自然科学青年基金项目、国家自然科学面上基金项目、航天科工集团横向课题、总装备部重大专项项目等10余项。在高超声速进气道不起动机理、状态监测、控制等方面共计发表论文80余篇，其中SCI检索60余篇。申报中国发明专利及国防发明专利20项，其中已授权15项。
主要学术任职
下列杂志的特约审稿人：
国内：《航空学报》、《航空动力学报》、《推进技术》、《固体火箭技术》；
国外：《Acta Astronautica》、《Journal of Propulsion and Power》、《ASCE's Journal of Aerospace Engineering》、《Aerospace Science and Technology》
国家自然基金评议专家
-----------------------------------------------------------------
发表学术论文
google 学术索引
论文期刊
已接收文章
序号
作者信息
论文题目及期刊信息
检索情况
86
Feng Shuo, Chang Juntao*, Yang Qingchun, Bao Wen*
Simulation study on modeling for design parameters analysis of free-piston tunnels. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS - PART G: JOURNAL OF AEROSPACE ENGINEERING. 2015: **1335.
SCI
2016年度
序号
作者信息
论文题目及期刊信息
检索情况
85
Hao Xinyue, Chang Juntao*, Bao Wen*, Zhang Zexu
A model of mode transition logic in dual-mode scramjet engines. AEROSPACE SCIENCE AND TECHNOLOGY. 2016, 49: 173-184.
SCI
2015年度
序号
作者信息
论文题目及期刊信息
检索情况
84
Xu Kejing*, Chang Juntao, Zhou Weixing, Yu Daren
Mechanism and prediction for occurrence of shock train sharp forward movement. 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3747.
EI
83
Zhang Chenlin*, Chang Juntao, Shi Wen, Bao Wen
Influence factor analysis of performance parameter for a strut/cavity supersonic combustor. 51st AIAA/SAE/ASEE Joint Propulsion Conference. AIAA 2015-3944.
EI
82Qi Yiwen*, Bao Wen, Chang, Juntao
Robust asynchronous bumpless transfer for switched linear systems. INTERNATIONAL JOURNAL OF CONTROL. 2015, 88(12): 2433-2443.
SCI
81
Zhang Cong, Qin Jiang*, Yang Qingchun, Zhang Silong, Chang Juntao, Bao Wen*
Indirect measurement method of inner wall temperature of scramjet with a state observer. ACTA ASTRONAUTICA. 2015, 115: 330-337.
SCI
80
Jiao Xiaoliang, Chang Juntao*, Wang Zhongqi, Yu Daren
Mechanism Study on Local Unstart of Hypersonic Inlet at High Mach Number. AIAA JOURNAL. 2015, 53(10): 3102-3112.
SCI
79
Zhang Cong, Yang Qingchun*, Chang Juntao, Tang Jingfeng , Bao Wen
Nonlinear Characteristics and detection of combustion Modes for a Hydrocarbon fueled scramjet. ACTA ASTRONAUTICA. 2015, 110: 89-98.
SCI
78
Chang Juntao*, Wang Lei, Qin Bin, Bao Wen, Yu Daren
Real-time unstart prediction and detection of hypersonic inlet based on recursive Fourier transform. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS - PART G: JOURNAL OF AEROSPACE ENGINEERING. 2015, 229(4): 772-778.
SCI
77
Yang Qingchun, Bao Wen*, Zong Youhai, Chang Juntao, Hu Jichao, Wu Meng
Combustion characteristics of a dual-mode scramjet injecting liquid kerosene by multiple struts. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS - PART G: JOURNAL OF AEROSPACE ENGINEERING. 2015, 229(6): 983-992.
SCI
76
Qi Yiwen*, Bao Wen, Chang Juntao
State-Based Switching Control Strategy with Application to Aeroengine Safety Protection. JOURNAL OF AEROSPACE ENGINEERING. 2015, 28(3): **.
SCI
75
Cao Ruifeng, Chang Juntao*, Tang Jingfeng, Bao Wen, Yu Daren, Wang Zhongqi
Switching control of thrust regulation and inlet unstart protection for scramjet engine based on strategy of integral initial values resetting. AEROSPACE SCIENCE AND TECHNOLOGY. 2015, 45: 484-489.
SCI
74
Cao Ruifeng, Chang Juntao*, Tang Jingfeng, Bao Wen, Yu Daren, Wang Zhongqi
Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy. AEROSPACE SCIENCE AND TECHNOLOGY. 2015, 40:96-103.
SCI
73
Qin Bin, Chang Juntao*, Jiao Xiaoliang, Bao Wen
Unstart Margin Characterization Method of Scramjet Considering Isolator–Combustor Interactions. AIAA JOURNAL. 2015, 53(2): 493-500.
SCI
72
Yang Qingchun, Shi Wen, Chang Juntao, Bao Wen*
Maximum thrust for the rocket-ejector mode of the hydrogen fueled rocket-based combined cycle engine. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY. 2015, 40(9): 3771-3776.
SCI
71
Yang Qingchun*, Chang Juntao, Zhang Duo, Hu Jichao, Bao Wen
Comment on " Parametric Ideal Scramjet Cycle Analysis ". JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER. 2015, 29(1): 203-204.
SCI Editorial Material
70
Zong Youhai, Bao Wen*, Chang Juntao, Hu Jichao, Yang Qingchun, Song Jian, Wu Meng
Effect of Fuel Injection Allocation on the Combustion Characteristics of a Cavity-Strut Model Scramjet. JOURNAL OF AEROSPACE ENGINEERING. 2015, 28(1): **.
SCI
69
Hu Jichao, Chang Juntao*, Qin Bin, Wang Lei, Bao Wen, Qin Jiang
Scramjwet Isolator Shock-Train Leading-Edge Position Modeling Based on Equilibrium Manifold. JOURNAL OF AEROSPACE ENGINEERING. 2015, 28(2): **.
SCI
68
Yang Qingchun, Hu Jichao, Chang Juntao, Zong Youhai, Bao Wen*
Experimental study on combustion mode transition effects in a strut-based scramjet combustor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2015, 229(4): 764-771.
SCI
2014年度
序号
作者信息
论文题目及期刊信息
检索情况
67
Bao Wen*, Hu Jichao, Zong Youhai, Yang Qingchun, Chang Juntao, Wu Meng, Yu Daren
Ignition Characteristics of a Liquid-Kerosene-Fueled Scramjet during Air Throttling Combined with a Gas Generator. JOURNAL OF AEROSPACE ENGINEERING. 2014, 27(5): ：**
SCI
66
Yang Qingchun, Chang Juntao, Bao Wen*
Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet. ENERGY. 2014, 76(552-558.
SCI
65
Yang Qingchun*, Chang Juntao, Bao Wen
Relative Time scale analysis for pressure propagation during ignition process of a scramjet. AEROSPACE SCIENCE AND TECHNOLOGY. 2014, 39(206-210.
SCI
64
Hu Jichao, Chang Juntao, Bao Wen*, Yang Qingchun, Wen John
Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection. ACTA ASTRONAUTICA. 2014, 104(1): 84-90.
SCI
63
Hu Jichao*, Bao Wen, Chang Juntao
Flame Transition in Dual-Mode Scramjet Combustor with Oxygen Piloted Ignition. JOURNAL OF PROPULSION AND POWER. 2014, 30(4): 1103-1107.
SCI
62
Cao Ruifeng, Chang Juntao*, Tang Jingfeng, Wang Zhongqi, Yu Daren*
Study on combustion mode transition of hydrogen fueled dual-mode scramjet engine based on thermodynamic cycle analysis. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY. 2014, 39(36): 21251-21258.
SCI
61
Chang Juntao*, Wang Lei, Bao Wen
Mathematical modeling and characteristic analysis of scramjet buzz. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2014, 228(13): 2542-2552.
SCI
60
Qin Bin, Chang Juntao*, Jiao Xiaoliang, Bao Wen, Yu Daren
Numerical investigation of the impact of asymmetric fuel injection on shock train characteristics. ACTA ASTRONAUTICA. 2014, 105(1): 66-74.
SCI
59
Chang Juntao*, Wang Lei, Bao Wen, Yang Qinchun, Qin Jiang
Experimental Investigation of Hysteresis Phenomenon for Scramjet Engine. AIAA JOURNAL. 2014, 52(2): 447-451.
SCI
58
Chang Juntao*, Zheng Risheng, Yu Daren, Bao Wen, Chen Fu, Jiang Weiyu, Zhu Shoumei, Zheng Riheng
Minimization of classification samples for supercritical and subcritical patterns of supersonic inlet. JOURNAL OF THERMAL SCIENCE. 2014, 23(4): 375-380.
SCI
57
Chang Juntao*, Zheng Risheng, Wang Lei, Bao Wen, Yu Daren
Backpressure unstart detection for a scramjet inlet based on information fusion. ACTA ASTRONAUTICA. 2014, 95: 1-14.
SCI
56
Yang Qingchun, Chang Juntao, Bao Wen*
Richtmyer-Meshkov Instability Induced Mixing Enhancement in the Scramjet Combustor with a Central Strut. ADVANCES IN MECHANICAL ENGINEERING. 2014, 2014: 614189.
SCI
55
Hu Jichao, Chang Juntao*, Bao Wen*
Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust. SCIENTIFIC WORLD JOURNAL. 2014, 2014: 675498
SCI
54
Yang Qingchun, Chang Juntao, Bao Wen*, Deng Jun
A mechanism of combustion mode transition for hydrogen fueled scramjet. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY. 2014, 39(18): 9791-9797.
SCI
53
Qi Yiwen*, Bao Wen, Zhao Jun, Chang Juntao
Coordinated control for regulation/protection mode-switching of ducted rockets. ACTA ASTRONAUTICA. 2014, 98: 138-146.
SCI
52
Bao Wen*, Zong Youhai, Chang Juntao, Hu Jichao, Yang Qingchun, Song Jian, Wu Meng
Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2014, 228(12): 2323-2328.
SCI
51
Bao Wen*, Zong Youhai, Chang Juntao, Yu Daren
Effect of structural factors on maximum aerodynamic heat flux of strut leading surface. APPLIED THERMAL ENGINEERING. 2014, 69(1-2): 188-198.
SCI
50
郑日升*，李伟鹏，常军涛，崔佃飞，满延进，朱守梅，于达仁，陈浮
"X"布局高超声速倒置进气道激波与附面层干扰抑制研究. 推进技术. 2014, 35(9): 1153-1161.
Suppression of interaction between shock wave and boundary layer for "X" hypersonic inverted inlet.
EI
49
Chang Juntao*, Cao Shibin, Zhang Junlong, Zhou Jianfeng, Bao Wen, Su Wenqing, Li Zhixin
Effects of Air Vitiation on Scramjet Performance Based on Thermodynamic Cycle Analysis. JAAE OPEN ACCESS. 2014, 3(1): **.
JAAE OPEN ACCESS
2013年度
序号
作者信息
论文题目及期刊信息
检索情况
48
Chang Juntao*, Li Bin, Bao Wen, Niu Wenyu, Yu Daren
Friction-Compensation Control of Gas-Flow Regulation for Ducted Rockets Based on Adaptive Dither Method. JOURNAL OF AEROSPACE ENGINEERING. 2013, 26(4): 715-720.
SCI
47
Hu Jichao, Chang Juntao*, Wang Lei, Cao Shibin, Bao Wen
Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet. SCIENTIFIC WORLD JOURNAL. 2013, 2013: 254376.
SCI
46
Cao Ruifeng, Chang Juntao*, Bao Wen*, Guo Manli, Qin Jiang, Yu Daren, Wang Zhongqi
Analysis of combustion mode and operating route for hydrogen fueled scramjet engine. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY. 2013, 38(14): 5928-5935.
SCI
45
Bao Wen*, Yang Qingchun, Chang Juntao, Zong Youhai, Hu Jichao
Dynamic Characteristics of Combustion Mode Transitions in a Strut-Based Scramjet Combustor Model. JOURNAL OF PROPULSION AND POWER. 2013, 29(5): 1244-1248.
SCI
44
Hu Jichao*, Qin Jiang, Chang Juntao, Bao Wen*, Zong Youhai, Yang Qingchun
Combustion stabilization based on a center flame strut in a liquid kerosene fueled supersonic combustor. JOURNAL OF THERMAL SCIENCE. 2013, 22(5): 497-504.
SCI
43
Bao Wen*, Hu Jichao, Zong Youhai, Yang Qingchun, Wu Meng, Chang Juntao, Yu Daren
Combustion characteristic using O-2-pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2013, 227(12): 1870-1880.
SCI
42
Bao Wen*, Qi Yiwen, Chang Juntao
Multi-objective regulating and protecting control for ducted rocket using a bumpless transfer scheme. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2013, 227(2): 311-325.
SCI
2012年度
序号
作者信息
论文题目及期刊信息
检索情况
41
Chang Juntao, Wang Lei, Bao Wen, Qin Jiang*, Niu Jun, Xue Wei
Novel Oscillatory Patterns of Hypersonic Inlet Buzz. JOURNAL OF PROPULSION AND POWER. 2012, 28(6): 1214-1221.
SCI
40
Chang Juntao, Li Bin, Bao Wen*, Yu Daren
Shock Train Leading-edge Detection in an Isolator Using Genetic Algorithm. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2012, 226(11): 1424-1431.
SCI
39
Chang Juntao*, Yu Daren, Bao Wen, Wang Cong, Chen Tianrui
Mathematical Modeling and Rapid Recognition of Hypersonic Inlet Buzz. AEROSPACE SCIENCE AND TECHNOLOGY. 2012, 23(1): 172-178.
SCI
38
Bao Wen*, Qi Yiwen, Zhao Jun, Chang Juntao
Robust dynamic bumpless transfer: an exact model matching approach. IET CONTROL THEORY AND APPLICATIONS. 2012, 6(10): 1341-1350.
SCI
37
Bao Wen*, Zong Youhai, Chang Juntao, Cui Tao
Effects of Strut Swept Angle on the Drag of Scramjet. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2012, 226(4): 455-466.
SCI
36
鲍文*，李伟鹏，常军涛，付海洋
基于遗传算法的高超声速进气道自动优化设计. 系统仿真学报. 2012, 24(4): 765-768.
Automated optimization design of hypersonic inlet using genetic algorithm.
2011年度
序号
作者信息
论文题目及期刊信息
检索情况
35
Chang Juntao*, Hu Qinghua, Yu Daren, Bao Wen
Classifier Utility Modeling and Analysis of Hypersonic Inlet Start/Unstart Considering Training Data Costs. ACTA ASTRONAUTICA. 2011, 69(9-10): 841-847.
SCI
34
Chang Juntao, Li Bin, Bao Wen, Niu Wenyu, Yu Daren*
Thrust Control System Design of Ducted Rockets. ACTA ASTRONAUTICA. 2011, 69(1-2): 86–95.
SCI
2010年度
序号
作者信息
论文题目及期刊信息
检索情况
33
Chang Juntao*, Fan Yi, Bao Wen, Yu Daren*, Shen Yi
Unstart Margin Control of Hypersonic Inlets. ACTA ASTRONAUTICA. 2010, 66(1-2): 78-87.
SCI
32
Shi X., Chang Juntao*, Bao Wen, Yu Daren, Li B
Supersonic Inlet Buzz Margin Control of Ducted Rocket. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2010, 224(10): 1131-1139.
SCI
31
Fan Yi*, Chang Juntao, Bao Wen, Yu Daren
Effects of Boundary Layer Bleeding on Unstart Oscillatory Flow of Hypersonic Inlets. AERONAUTICAL JOURNAL. 2010, 114(1157): 445-450.
SCI
30
Niu Wenyu, Bao Wen*, Chang Juntao, Cui Tao, Yu Daren*
Control System Design and Experiment of Needle-Type Gas Regulating System for Ducted Rocket. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2010, 224(5): 563-573.
SCI
29
Yao Zhaohui, Bao Wen*, Chang Juntao, Yu Daren, Tang Jingfeng
Modelling for Couplings of an Airframe-Propulsion Integrated Hypersonic Vehicle with Engine Safety Boundaries. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2010, 224(1): 43-55.
SCI
28
Bao Wen, Li Bin, Chang Juntao, Niu Wenyu, Yu Daren*
Switching control of thrust regulation and inlet buzz protection for ducted rocket. ACTA ASTRONAUTICA. 2010, 67(7-8): 764-773.
SCI
27
于达仁*，常军涛，崔涛，唐井峰，鲍文
超燃冲压发动机控制方法. 推进技术. 2010, 31(6): 764-772.
Control method of scramjet engines.
EI
2009年度
序号
作者信息
论文题目及期刊信息
检索情况
26
Chang Juntao*, Yu Daren, Bao Wen, Fan Yi
Operation Pattern Classification of Hypersonic Inlets. ACTA ASTRONAUTICA. 2009, 65(3-4): 457-466.
SCI
25
Chang Juntao*, Bao Wen, Yu Daren, Fan Yi, Shen Yi
Effects of Wall Cooling on Performance Parameters of Hypersonic Inlets. ACTA ASTRONAUTICA. 2009, 65(3-4): 467-476.
SCI
24
Chang Juntao*, Yu Daren, Bao Wen, Xie Zongxia, Fan Yi
A CFD Assessment of Classifications for Hypersonic Inlet Start/Unstart Phenomena. AERONAUTICAL JOURNAL. 2009, 113(1142): 263-271.
SCI
23
Chang Juntao*, Yu Daren, Bao Wen, Fan Yi, Shen Yi
Effects of Boundary Layers Bleeding on Unstart/Restart Characteristics of Hypersonic Inlets. AERONAUTICAL JOURNAL. 2009, 113(1143): 319-327.
SCI
22
Chang Juntao*, Bao Wen, Yu Daren, Fan Yi, Shen Yi, Zhou Weixing
Hypersonic Inlet Control with Pulse Periodic Energy Addition. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2009, 223(2): 85-94.
SCI
21
Chang Juntao*, Bao Wen, Fan Yi, Yu Daren*
Performance Optimization of Hypersonic Inlets with Pulse Periodic Energy Addition. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2009, 223(6): 691-699.
SCI
20
Chang Juntao*, Fan Yi
Effects of Boundary Layers Bleeding on Performance Parameters of Hypersonic Inlets. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY. 2009, 81(3): 204-211.
SCI
19
Cui Tao*, Yu Daren, Chang Juntao, Bao Wen
Catastrophe Model for Supersonic Inlet Start/Unstart. JOURNAL OF AIRCRAFT. 2009, 46(4): 1160-1166.
SCI
18
范轶*，常军涛，鲍文
壁面温度对高超声速进气道不起动/再起动特性的影响. 固体火箭技术. 2009, 32(3): 266-270.
Effects of wall temperature on unstart/restart characteristics of hypersonic inlets.
EI
17
常军涛*，于达仁，鲍文，曲亮
楔面转折角对高超声速进气道不起动/再起动特性的影响. 固体火箭技术. 2009, 32(2): 2135-140.
Effects of turning angles of wedge on unstart/restart characteristics of hypersonic inlets.
EI
2008年度
序号
作者信息
论文题目及期刊信息
检索情况
16
Chang Juntao*, Yu Daren, Bao Wen, Qu Liang
Dimensionless Analysis of the Unstart Boundary for 2D Mixed Hypersonic Inlets. AERONAUTICAL JOURNAL. 2008, 112(1135): 547-555.
SCI
15
Cui Tao*, Yu Daren, Chang Juntao, Bao Wen
Topological Geometry Interpretation of Supersonic Inlet Start/Unstart Based on Catastrophe Theory. JOURNAL OF AIRCRAFT. 2008, 45(4): 1464-1468.
SCI
14
Chang Juntao*, Yu Daren, Bao Wen, Qu Liang
Influence Factors of Unstart Boundary for Hypersonic Inlets. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2008-4586.
EI
13
常军涛*，鲍文，崔涛，于达仁
抽吸对高超声速进气道抗反压能力的影响. 航空动力学报. 2008, 23(3): 505-509.
Effect of suctions on maximum backpressure ratios of hypersonic inlets.
EI
12
常军涛*，于达仁，鲍文
攻角引起的高超声速进气道不起动/再起动特性分析. 航空动力学报. 2008, 23(5): 816-821.
Characteristic analysis of unstart/restart of hypersonic inlets caused by variations of attack angle of freestream.
EI
11
鲍文*，李伟鹏，常军涛，付海洋
基于FLUENT_MATLAB接口的分布参数系统闭环控制仿真. 系统仿真学报. 2008, 20(11): 2851-2854+2858.
Closed-loop Control Simulation Technology of Distributed Parameter System Based on FLUENT/MATLAB Interface.
EI pageone
10
于达仁*，何保成，吕晓武，常军涛
旋转冲压发动机进气道压比特性分析. 推进技术. 2008, 29(3): 329-333.
Characteristics analysis of pressure ratios for rotated ramjet inlets.
EI
2007年度
序号
作者信息
论文题目及期刊信息
检索情况
9
Yu Daren*, Chang Juntao, Bao Wen, Xie Zongxia
Optimal classification criterions of hypersonic inlet start/unstart. JOURNAL OF PROPULSION AND POWER. 2007, 23(2): 310-316.
SCI
8
何保成*，常军涛，于达仁
冲压发动机进气道不起动边界分析. 推进技术. 2007, 28(3): 269-272.
Analysis of the unstart boundary for ramjet inlets.
EI
7
何保成*，姚照辉，鲍文，常军涛
基于SIMULINK的超声速进气道仿真方法. 推进技术. 2007, 28(2): 199-203.
A simulation method based on SIMULINK for a supersonic inlet.
EI
6
常军涛*，鲍文，于达仁，曲亮
一维超声速进气道运动激波的动态仿真. 导弹与航天运载技术. 2007, 4: 48-51.
Dynamics simulations of shock-motion of one-dimensional supersonic inlets.
2006年度
序号
作者信息
论文题目及期刊信息
检索情况
5
Chang Juntao*, Bao Wen
Observers Design for Shock Position of Supersonic Inlet Based on Equilibrium Manifold. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA 2006-4305.
EI
4
He Baocheng*, Chang Juntao, Bao Wen, Yu Daren
Supersonic Inlet Dynamics Model Based on Equilibrium Manifold. 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference. AIAA 2006-7903.
EI
2005年度
序号
作者信息
论文题目及期刊信息
检索情况
3
鲍文*，常军涛，郭新刚，崔涛
超燃冲压发动机进气道不起动仿真研究. 航空动力学报. 2005, 20(5): 731-735.
Unstart Simulation of Scramjet Inlets.
EI
2
鲍文*，常军涛，牛文玉，于达仁
超燃冲压发动机磁控进气道设计影响因素分析. 航空动力学报. 2005, 20(3): 368-372.
Influence Factor Analysis of the MHD Controlled Scramjet Inlet Design.
EI
1
鲍文*，常军涛，马照祥，于达仁
涡扇发动机转速鲁棒控制器设计及试验. 推进技术. 2005, 26(2): 158-161.
Robust controller design and experiment of turbofan.
EI
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研究领域
研究领域
研究内涵
高超声速冲压发动机控制
研究问题主要包括：面向控制的发动机建模、发动机多变量控制、发动机鲁棒控制
高超声速进气道状态监测
研究问题主要包括：进气道不起动监测方法、多种不起动模式转换机理、进气道再起动控制
超声速燃烧组织及燃烧模态机理
研究问题主要包括：燃烧室性能优化、燃烧模态转换机理、燃烧模态识别和控制
科研项目
xxx发动机控制xxx2013年7月~负责人横向项目
xxx燃烧特性xxx2012年7月~负责人纵向项目
多模块高超声速进气道不起动耦合特性及失稳机理研究国家自然科学基金2010年1月~2012年12月负责人纵向项目
燃烧过程对高超声速进气道不起动的影响机理研究国家自然科学基金2014年1月~负责人纵向项目
奖项成果
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讲授课程
课题名称授课对象
《空间推进技术》研究生
《超燃冲压发动机研究前沿》本科生
招生信息
硕士招生:
欢迎对超燃冲压发动机感兴趣的同学报考、联系。具有工程热力学、流体力学、空气动力学等基本专业知识。
博士招生:
欢迎对超燃冲压发动机感兴趣的同学报考、联系。具有工程热力学、流体力学、空气动力学等基本专业知识。
