基本信息论文专著硕博士研究生
奖项成果
2017年，第三届“兴洲奖”获得者 2017年，国防技术发明二等奖（排序第一） 2017年，国家自然科学优秀青年基金 2015年，教育部科学技术进步一等奖 2015年，入选哈尔滨工业大学“青年拔尖教授”计划 2014年，黑龙江省自然科学二等奖


教育与工作经历


1998年09月-2002年07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09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03月-2010年12月，哈尔滨工业大学基础与交叉科学研究院，讲师 2010年12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 2015年12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 2017年08月-至今，哈尔滨工业大学基础与交叉科学研究院， 获得“国家自然科学优秀青年基金”

讲授课程
本科生课程：高超推进原理 研究生课程：空间推进技术、热力系统控制进展


主要学术任职
《空气动力学报》和《实验流体力学》青年编委 Associate editor,《Advances in Aircraft and Spacecraft Science》,ESCI期刊Associate editor,《Aeronautics & Aerospace Engineering》Associate editor,《American Journal of Aerospace Engineering》Associate editor,《International Journal of Aerospace Engineering and Technology 》航天第三专业信息网发动机控制组专业委员会委员
中国工程热物理学会热机气动热力学分会青年委员会委员
激波与激波管专业委员会超声速内流专业组成员 第8届全国高超声速科学技术会议组委会大会执行副主席


招生信息
本科招生:（每年若干名），热爱学习，愿意钻研和从事科技创新实践活动，高超声速推进相关。 硕士招生:（每年2名），能积极主动学习，具有一定的创新思维。超燃冲压发动机内部流动机理及其控制、航空发动机控制。具有工程热力学、流体力学、空气动力学、控制理论等基本专业知识。 博士招生:（每年1~2名），积极主动，勤奋刻苦，思维活跃，具有工程热物理或者控制学科背景。超燃冲压发动机内部流动机理及其控制、航空发动机控制。具有工程热力学、流体力学、空气动力学、控制理论等基本专业知识。


论文专著

2019年度


130. Junlong Zhang, Juntao Chang*, Fuxu Quan, Liqian Bian, Wen Bao, Ignition characteristics in a thin strut-equipped dual mode combustor fueled with liquid kerosene, Acta Astronautica, 2019, 161:125-138

129. Ziao Wang, Juntao Chang*, Nan Li, Kejing Xu, Experimental investigation of the throttling process and oscillation mechanism in a supersonic cascade, AIP Advances, 2019,9:055103

128. Jicheng Ma, Juntao Chang*, QingPing Huang, Wen Bao, Daren Yu, Multi-objective coordinated control of regeneratively-cooled scramjet engine with two-stage kerosene injection, Aerospace Science and Technology, 2019, 90:59-69
127. Wen Shi, Juntao Chang*, Junlong Zhang, Jicheng Ma, Ziao Wang, Wen Bao. Numerical investigation on the forced oscillation of shock train in hypersonic inlet with translating cowl, Aerospace Science and Technology, 2019, 87:311-322

126. Wen Shi, Juntao Chang*, Jicheng Ma, Youyin Wang, Lin Gao, Wen Bao. Path dependence characteristic of shock train in a 2D hypersonic inlet with variable background waves, Aerospace Science and Technology, 2019, 86:650-658

125. Nan Li, Juntao Chang*, Kejing Xu, Daren Yu, Yanping Song. Closed-loop control of shock train in inlet-isolator with incident shocks, Experimental Thermal and Fluid Science, 2019, 103:355-363

124. Junlong Zhang, Juntao Chang*, Jicheng Ma, Youyin Wang, Wen Bao. Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut, Aerospace Science and Technology, 2019, 84:686-697

123. Wen Shi, Juntao Chang*, Youyin Wang, Wen Bao, Xiaoyong Liu. Buzz evolution process investigation of a two-ramp inlet with translating cowl, Aerospace Science and Technology, 2019, 84:712-723

122. Jialin Zheng, Juntao Chang*, Shengbo Yang, Xinyue Hao, Daren Yu. Trajectory optimization for a TBCC-powered supersonic vehicle with transition thrust pinch, Aerospace Science and Technology , 2019, 84:214-222

121. Jicheng Ma, Juntao Chang*, Junlong Zhang, Wen Bao, Daren Yu. Control-oriented unsteady one-dimensional model for a hydrocarbon regeneratively-cooled scramjet engine, Aerospace Science and Technology , 2019, 85:158-170

2018年度

120. Juntao Chang*, Junlong Zhang, Wen Bao, Daren Yu. Research progress on strut-equipped supersonic combustors for scramjet application, Progress in Aerospace Sciences, 2018, 103:1-30

119. Jicheng Ma, Juntao Chang*, Junlong Zhang, Wen Bao, Daren Yu. Control-oriented modeling and real-time simulation method for a dual-mode scramjet combustor , Acta Astronautica, 2018, 153:82-94

118. Jialin Zheng, Juntao Chang*, Jicheng Ma, Daren Yu. Performance uncertainty propagation analysis for control-oriented model of a turbine-based combined cycle engine, Acta Astronautica, 2018, 153:39-49

117. Nan Li, Juntao Chang*, Kejing Xu, Daren Yu, Wen Bao, Yanping Song. Oscillation of the shock train in an isolator with incident shocks, Physics of Fluids, 30, 116102 (2018)

116. Ziao Wang, Juntao Chang*, Junlong Zhang, Jicheng Ma. Investigations on flowfield behavior and resistance backpressure characteristics of supersonic cascade with boundary layer suction, Acta Astronautica, 2018, 152:588-601

115. Wen Shi, Juntao Chang*, Junlong Zhang, Youyin Wang, Wenxin Hou, Wen Bao. Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl, Acta Astronautica, 2018, 152:682-691

114. Kejing Xu, Juntao Chang*, Nan Li, Weixing Zhou, Daren Yu. Preliminary investigation of limits of shock train jumps in a hypersonic inlet-isolator, European Journal of Mechanics / B Fluids, 2018, 72:664-675

113. Chenlin Zhang, Juntao Chang*, Shuo Feng, Wen Bao, Daren Yu. Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor, Aerospace Science and Technology , 2018, 80:496–507

112. Nan Li, Juntao Chang*, Jingfeng Tang, Daren Yu, Wen Bao, Yanping Song. Effect of control route on the unstart/restart characteristics of an over-under TBCC inlet, Advances in Aircraft and Spacecraft Science, 2018, 5:431-444

111. Kejing Xu, Juntao Chang*, Nan Li, Weixing Zhou, Daren Yu. Experimental investigation of mechanism and limits for shock train rapid forward movement, Experimental Thermal and Fluid Science, 2018, 98:336-345

110. Xinyu Zhao, Jinfu Liu*, Daren Yu*, Juntao Chang. One-day-ahead probabilistic wind speed forecast based on optimized numerical weather prediction data, Energy Conversion and Management, 2018, 164:560-569

109. Jingxue Ma, Juntao Chang*, Jicheng Ma, Wen Bao, Daren Yu. Mathematical modeling and characteristic analysis for over-under turbine based combined cycle engine, Acta Astronautica, 2018, 148:141-152.

108. Chenlin Zhang, Juntao Chang*, Junlong Zhang, Wen Bao, Daren Yu. Effect of continuous Mach number variation of incoming flow on ram-scram transition in a dual-mode combustor, Aerospace Science and Technology, 2018, 76:433-441.

107. Junlong Zhang, Juntao Chang*, Wen Shi, Wenxin Hou, Wen Bao. Combustion stabilizations in a liquid kerosene fueled supersonic combustor equipped with an integrated pilot strut, Aerospace Science and Technology, 2018, 77:83-91.

106. Junlong Zhang, Juntao Chang*, Jicheng Ma, Yuanshi Zhang, Wen Bao. Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut, Aerospace Science and Technology, 2018, 76:49-57.

105. Chenlin Zhang, Juntao Chang*, Jingxue Ma, Wen Bao, Daren Yu, Jingfeng Tang. Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor, Aerospace Science and Technology, 2018, 72:516-524.

104. Jiao Xiaoliang*, Chang Juntao**, Wang Zhongqi, Yu Daren. Periodic forcing of a shock train in a scramjet inlet-isolator at overspeed condition, Acta Astronautica, 2018, 143:244-254.

103. Li Nan, Chang Juntao, Jiang Chenzhong, Yu Daren, Bao Wen, Song Yanping, Jian Xiaoliang*. Unstart/restart hysteresis characteristics analysis of an over–under TBCC inlet caused by backpressure and splitter. Aerospace Science and Technology, 2018, 72: 418-425.

2017年度

102. Li Nan, Chang Juntao*, Xu Kejing, Yu Daren, Bao Wen, Song Yanping. Prediction dynamic model of shock train with complex background waves. Physics of Fluids 29, 116103 (2017); https://doi.org/10.1063/1.**.

101. Zhang Junlong, Chang Juntao*, Ma Jicheng, Zhang Chenlin, Bao Wen . Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut. Aerospace Science and Technology, 2017, 70: 152-160.

100. Xu Kejing, Chang Juntao*, Zhou Weixing, Yu Daren . Mechanism of shock train rapid motion induced by variation of attack angle. Acta Astronautica, 2017, 140: 18-26.

99. Feng Shuo, Chang Juntao*, Zhang Yuanshi, Zhang Chenlin, Wang Youyin, Bao Wen. Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle. Aerospace Science and Technology, 2017, 68: 320-330.

98. Zhang Chenlin, Chang Juntao*, Feng Shuo, Ma Jicheng, Zhang Junlong, Bao Wen. Pressure rising slope variation accompanying with combustion mode transition in a dual-mode combustor. Aerospace Science and Technology, 2017, 68: 370-379.

97. Feng Shuo, Chang Juntao*, Zhang Chenlin, Wang Youyin, Ma Jicheng, Bao Wen. Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor. Aerospace Science and Technology, 2017, 67: 96-104.

96. Zhang Chenlin, Chang Juntao*, Zhang Yuanshi, Wang Youyin, Bao Wen. Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor. Acta Astronautica, 2017, 137: 44-51.

95. Feng Shuo, Chang Juntao*, Zhang Junlong, Zhang Chenlin, Bao Wen. Numerical and experimental investigation of improving combustion performance of variable geometry dual-mode combustor. Aerospace Science and Technology, 2017, 64: 213-222.

94. Zhang Chenlin, Chang Juntao*, Liu MengMeng, Feng Shuo, Shi Wen, Bao Wen. Effect of heat release on movement characteristics of shock train in an isolator. Acta Astronautica, 2017, 133: 185-194.

93. Jiao Xiaoliang, Chang Juntao*, Wang Zhongqi, Yu Daren. Numerical Study on Hypersonic Nozzle-Inlet Starting Characteristics in a Shock Tunnel. Acta Astronautica, 2017, 130: 167-179.

92. Chang Juntao*, Li Nan, Xu Kejing, Bao Wen, Yu Daren. Recent Research Progress on unstart mechanism, detection and control of hypersonic inlet. Progress in Aerospace Sciences, 2017, 89: 1-22.

91. Li Nan, Chang Juntao*, Yu Daren, Bao Wen, Song Yanping. Mathematical Model of Shock Train Path with Complex Background Waves. Journal of Propulsion and Power, 2017: 33(2): 468-478.

2016年度

90. He Yubao, Chang Juntao, Bao Wen, Huang Hongyan, Yu Daren. Numerical Investigation of Local Resistance to Backpressure in Hypersonic Inlet with Suction. Journal of Propulsion and Power, 2016, 32(6): 1531-1543.

89. Cao Ruifeng, Cui Tao, Yu Daren, Chang Juntao, Bao Wen, Wang Zhongqi. New Method for Solving One-Dimensional Transonic Reacting Flows of a Scramjet Combustor. Journal of Propulsion and Power, 2016, 32(6): 1403-1412.

88. Jiao Xiaoliang, Chang Juntao*, Wang Zhongqi, Yu Daren. Hysteresis phenomenon of hypersonic inlet at high Mach number. Acta Astronautica, 2016, 128: 657-668.

87. Jiao Xiaoliang, Chang Juntao*, Wang Zhongqi, Yu Daren. Investigation of hypersonic inlet pulse-starting characteristics at high Mach number. Aerospace Science and Technology, 2016, 58: 427-436.

86. Xu Kejing*, Chang Juntao*, Zhou Weixing, Yu Daren. Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward Movement. AIAA Journal, 2016, 54(1): 1403-1412.

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.

2015年度

84. 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. 2016: 230(12): 2330-2342.

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.

82. Qi Yiwen*, Bao Wen, Chang, Juntao. Robust asynchronous bumpless transfer for switched linear systems. International Journal of Control. 2015, 88(12): 2433-2443.

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.

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.

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.

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.

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.

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): **.

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.

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.

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.

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.

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. 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): **.

69. Hu Jichao, Chang Juntao*, Qin Bin, Wang Lei, Bao Wen, Qin Jiang. Scramjet Isolator Shock-Train Leading-Edge Position Modeling Based on Equilibrium Manifold. Journal of Aerospace Engineering. 2015, 28(2): **.

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.

2014年度

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): ：**

66. Yang Qingchun, Chang Juntao, Bao Wen*. Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet. Energy. 2014, 76:552-558.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

55. Hu Jichao, Chang Juntao*, Bao Wen*. Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust, Entific World Journal. 2014, 2014: 675498

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.

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.

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.

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.

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): **.

2013年度

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.

47. Hu Jichao, Chang Juntao*, Wang Lei, Cao Shibin, Bao Wen. Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet, Entific World Journal. 2013, 2013: 254376.

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.

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.

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.

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.

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.

2012年度

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.

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.

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.

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.

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.

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

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.

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.

2010年度

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.

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.

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.

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.

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.

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.

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..

2009年度

26. Chang Juntao*, Yu Daren, Bao Wen, Fan Yi. Operation Pattern Classification of Hypersonic Inlets. Acta Astronautica. 2009, 65(3-4): 457-466.

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.

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.

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.

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.

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.

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.

19. Cui Tao*, Yu Daren, Chang Juntao, Bao Wen. Catastrophe Model for Supersonic Inlet Start/Unstart. Journal of Aircraft. 2009, 46(4): 1160-1166.

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.

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.

2008年度

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.

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.

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.

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.

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.

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.

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.

2007年度

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.

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..

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..

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

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.

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.

2005年度

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

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

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


毕业生及去向
博士生：

2010级博士，郑日升，研究方向：进气道气动设计；航天二院工作

2010级博士，杨庆春，研究方向：几何可调发动机；北航留校工作

2012级博士，焦晓亮，研究方向：不起动多模式；航天科工九院

2013级博士，丰硕，研究方向：几何可调燃烧室；航天科工三院

2014级博士，张辰琳，研究方向：燃烧模态转换机理；沈阳601所

2014级博士，徐珂靖，研究方向：激波串运动特性；

2014级博士，李楠，研究方向：激波串监测及控制；

2015级博士，马继承，研究方向：主动冷却发动机控制；

2015级博士，张军龙，研究方向：超声速燃烧火焰传播特性；

2016级博士，王子傲，研究方向：超声速叶片流动机理；

2016级博士，侯文新，研究方向：激波串运动机理；

2016级博士，郑佳琳，研究方向：组合发动机控制；

2017级博士，孔辰，研究方向：智能隔离段；

2018级博士，李云飞，研究方向：智能叶片；

硕士生：


2010级硕士，李斌，研究方向：多模块进气道耦合机理；美国攻读博士学位（已毕业）

2011级硕士，王磊，研究方向：不起动监测；北京301研究所

2012级硕士，秦斌，研究方向：激波串演化机理；哈工大深圳研究生院攻读博士学位

2013级硕士，曹石彬，研究方向：组合进气道；德国亚琛大学攻读博士学位

2013级硕士，周建峰，研究方向：燃烧模态；桑顿能源

2014级硕士，尹朝林，研究方向：组合发动机；中广核

2015级硕士，江晨钟，研究方向：组合发动机建模；美的集团

2016级硕士，马婧雪，研究方向：多模式协调控制；深圳招商银行

2017级硕士，吕铖坤，研究方向：航空发动机控制；

2017级硕士，罗超超，研究方向：进气道特性建模；

2018级硕士，孙晓雪，研究方向：航空发动机控制；

2018级硕士，董义磊，研究方向：激波串监测和控制；

2018级硕士，黄庆平，研究方向：组合发动机控制