近期论文
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代表性学术专著
常军涛; 刘小勇; 鲍文; 于达仁; 高超声速进气道流动失稳机理及其控制, 科学出版社, 2021.
于达仁; 常军涛; 曹瑞峰; 杨晟博; 唐井峰; 鲍文; 超燃冲压发动机控制, 国防工业出版社, 2019.
代表性期刊论文
Li Nan, Chang Juntao*, Xu Kejing, Yu Daren, Bao Wen, Instability of shock train behavior with incident shocks. Journal of Fluid Mechanics 907, A40 (2021)
Ziao Wang, Juntao Chang*, Chen Kong, Renzhe Huang, and Xuanan Xin. Experimental investigation of micro-ramp control for shock train under various incoming flow conditions. Physical Review Fluids, 2022, 7(10): 103401.
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.
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
Chengkun Lv, Juntao Chang*, Wen Bao, and Daren Yu. Recent research progress on airbreathing aero-engine control algorithm. Propulsion and Power Research, 2022, 11(1): 1-57.
Yunfei Li, Juntao Chang*, Chen Kong, and Wen Bao. Recent progress of machine learning in flow modeling and active flow control. Chinese Journal of Aeronautics, 2022, 35(4): 14-44.
Ziao Wang, Kejing Xu and Juntao Chang*. Distributed Fluidic Control Method for Alleviating Rapid Movement of Shock Train. AIAA Journal, 2022, 60(11): 6252-6269.
Ziao Wang, Juntao Chang*, Chen Kong, Yunfei Li. Micro-ramp control for shock train structure and oscillation, AIAA Journal, 2021, 59(12): 4881-4904.
Li Nan, Chang Juntao*. Hysteretic Behaviors of Separation-Shock Driven by Backpressure in Isolator with Incident Shocks. AIAA Journal, 2021, 59(3): 960-971.
Chen Kong, Chenlin Zhang, Ziao Wang, Yunfei Li and Juntao Chang*. Efficient Prediction of Supersonic Flowfield in an Isolator Based on Pressure Sequence. AIAA Journal, 2022, 60(5): 2826-2835.
Chen Kong, Juntao Chang*, Nan Li, and Yunfei Li. Flowfield reconstruction and shock train leading edge detection in scramjet isolators. AIAA Journal, 2020, 58(9): 4068-4080.
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.
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.
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.
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.
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.
Ziao Wang, Juntao Chang*, Wenxin Hou and Daren Yu. Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves. Physics of Fluids, 2020, 32, 056105 (封面文章)
Ziao Wang, Juntao Chang*, Yiming Li, Ruoyu Chen, Wenxin Hou, Jifeng Guo and Lianjie Yue. Oscillation of the shock train under synchronous variation of incoming Mach number and backpressure. Physics of Fluids, 2022, 34: 046104.
Ziao Wang, Juntao Chang*, Guang Wu and Daren Yu. Experimental investigation of shock train behavior in a supersonic isolator. Physics of Fluids, 2021, 33, 046103
Yunfei Li, Ziao Wang*, Weiyu Jiang, Zongqi Xie, Chen Kong, and Juntao Chang*. Research on time sequence prediction of the flow field structure of supersonic cascade channels in wide range based on artificial neural network. Physics of Fluids, 2022, 34: 016106.
Yunfei Li, Juntao Chang*, Ziao Wang, and Chen Kong. An efficient deep learning framework to reconstruct the flow field sequences of the supersonic cascade channel. Physics of Fluids, 2021, 33, 056106.
Chen Kong, Juntao Chang*, Yunfei Li and Ziao Wang. A deep learning approach for the velocity field prediction in a scramjet isolator. Physics of Fluids, 2021, 33, 026103
Yunfei Li, Juntao Chang*, Ziao Wang, Chen Kong, Inversion and reconstruction of supersonic cascade passage flow field based on a model comprising transposed network and residual network, Physics of Fluids, 2019, 31, 126102.
Chen Kong, Ziao Wang, Junlong Zhang, Xuan Wang, Kai Wang, Yunfei Li and Juntao Chang*. Research on flame prediction in a scramjet combustor using data-driven model. Physics of Fluids, 2022, 34: 066101.
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, 2018, 30, 116102.
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, 2017, 29, 116103.
Ziao Wang, Juntao Chang*, Wenxin Hou, Daren Yu. Throttling process of a supersonic cascade studied by high-frequency response pressure and high-speed schlieren, Scientific Reports, 2021, 11, 13550
Chengkun Lv, Qian Huang, Juntao Chang*, Ziao Wang, Jialin Zheng, and Daren Yu. Mode transition path optimization for turbine-based combined-cycle ramjet stage under uncertainty propagation of integrated airframe-propulsion system. Energy, 2023: 126718.
Chengkun Lv, Haiqi Xu, Juntao Chang*, Youyin Wang, Ruoyu Chen, and Daren Yu. Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor. Energy, 2022, 261: 125324.
Chengkun Lv, Haiqi Xu, Fuxu Quan, Juntao Chang*, and Daren Yu. Thermodynamic modeling and analysis of ammonia injection pre-compressor cooling cycle: A novel scheme for high Mach number turbine engines. Energy Conversion and Management, 2022, 265: 115776.
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