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第一作者SCI论文
Wang Ziao,Chang Juntao*, Hou Wenxin, Yu Daren. Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves[J]. Physics of Fluids, 2020, 32: 056105. (SCI收录, DOI: 10.1063/5.0007400, IF=4.980, 期刊封面文章，流体力学顶级期刊)
Wang Ziao, Chang Juntao*, Wu Guangwei, Yu Daren. Experimental investigation of shock train behavior in a supersonic isolator[J]. Physics of Fluids, 2021, 33: 046103. (SCI收录, DOI: 10.1063/5.0047665, IF=4.980)
Wang Ziao, Chang Juntao*, Li Yiming, Chen Ruoyu, Hou Wenxin, Guo Jifeng, Yue Lianjie. Oscillation of the shock train under synchronous variation of incoming Mach number and backpressure[J]. Physics of Fluids, 2022, 34: 046104. (SCI收录, DOI: 10.1063/5.0087526, IF=4.980)
Wang Ziao, Chang Juntao*, Kong Chen, Huang Renzhe, Xin Xuanan. Experimental investigation of micro-ramp control for shock train under various incoming flow conditions[J]. Physical Review Fluids, 2022, 7: 103401. (SCI收录, DOI: 10.1103/PhysRevFluids.7.103401, IF=2.895, 流体力学顶级期刊)
ang Ziao,Chang Juntao*, Kong Chen, Li Yunfei. Micro-ramp control for shock train structure and oscillation[J]. AIAA Journal, 2021, 59(12): 4881-4904. (SCI收录, DOI: 10.2514/1.J062020, IF=2.624,航空航天领域权威期刊)
ang Ziao,Xu Kejing, Chang Juntao*. Distributed fluidic control method for alleviating rapid movement of shock train[J]. AIAA Journal, 2022, 60(11): 6252-6269. (SCI收录, DOI: 10.2514/1.J062020, IF=2.624)
Wang Ziao, Chang Juntao*, Li Yunfei, Kong Chen. Investigation of shock wave control by suction in a supersonic cascade[J]. Aerospace Science and Technology, 2021, 108: 105382. (SCI收录, DOI：10.1016/j.ast.2020.106382, IF=5.457)
Wang Ziao, Chang Juntao*, Zhang Junlong, Yu Daren. Evolution of subsonic and supersonic corner vortices in a supersonic cascade[J]. Aerospace Science and Technology, 2019, 95: 105509. (SCI收录, DOI: 10.1016/j.ast.2019.105509, IF=5.457)
Wang Ziao, Huang Renzhe, Li Yiming, Zheng Jialin, Guo Jifeng, Chang Juntao*. Experimental and numerical simulation of shock train characteristics in an isolator with incident shocks[J]. Aerospace Science and Technology, 2023, 138: 108309. (SCI收录, DOI: 10.1016/j.ast.2023.108309, IF=5.457)
Wang Ziao, Chang Juntao*, Zhang Junlong, Ma Jicheng. Investigations on flowfield behavior and resistance backpressure characteristics of supersonic cascade with boundary layer suction[J]. Acta Astronautica, 2018, 152: 588-601. (SCI收录, DOI: 10.1016/j.actaastro.2018.09.004, IF=2.954)
Wang Ziao, Chang Juntao*, Wu Guangwei, Hou Wenxin. Mechanism and detection of oscillatory flow in a supersonic cascade[J]. Acta Astronautica, 2021, 182: 77-99. (SCI收录, DOI: 10.1016/j.actaastro.2021.02.009, IF=2.954)
Wang Ziao, Xin Xuanan, Huang Renzhe, Kong Chen, Lv Chengkun, Chang Juntao*. Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels[J]. Acta Astronautica, 2022, 199: 232-248. (SCI收录, DOI: 10.1016/j.actaastro.2022.07.057, IF=2.954)
Wang Ziao, Xin Xuanan, Guo Jifeng, Yue Lianjie, Kong Chen, Huang Renzhe, Chang Juntao*. Hysteresis behavior of shock train driven by continuous incoming Mach number variation in an isolator with background waves[J]. European Journal of Mechanics / B Fluids, 2023, 101: 42-58. (SCI收录, DOI: j.euromechflu.2023.04.013, IF=2.598, 流体力学高水平期刊)
Wang Ziao, Chang Juntao*, Hou Wenxin, Yu Daren. Throttling process of a supersonic cascade studied by high-frequency response pressure and high-speed schlieren[J]. Scientific Reports, 2021, 11: 13550. (SCI收录, DOI: 10.1038/s41598-021-93021-1, IF=4.996)
Wang Ziao, Chang Juntao*, Li Nan, Xu Kejing. Experimental investigation of the throttling process and oscillation mechanism in a supersonic cascade[J]. AIP Advances, 2019, 9: 055103. (SCI收录, DOI: 10.1063/1.5093786, IF=1.697)
Wang Ziao, Chang Juntao*, Hou Wenxin, Yu Daren. Propagation of shock-wave/boundary-layer interaction unsteadiness in attached and separated flows[J]. AIP Advances, 2020, 10: 105011. (SCI收录, DOI: 10.1063/5.0023935, IF=1.697)
Wang Ziao, Xin Xuanan, Chen Ruoyu, Huang Renzhe, Kong Chen, Chang Juntao*. Development and evolution mechanism of streamwise vortex in an inward-turning inlet[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Accepted.
通讯作者SCI论文
Li Yunfei,Wang Ziao*, Jiang Weiyu, Xie Zongqi, Kong Chen, Chang Juntao. Research on time sequence prediction of the flow field structure of supersonic cascade channels in wide range based on artificial neural network[J]. Physics of Fluids, 2022, 34: 016106. (SCI收录, DOI: 10.1063/5.0073109, IF=4.980)
Kong Chen, Zhang Chenlin,Wang Ziao*, Li Yunfei, Chang Juntao. Efficient prediction of supersonic flowfield in an isolator based on pressure sequence[J]. AIAA Journal, 2022, 60(5): 2826-2835. (SCI收录, DOI: 10.2514/1.J061375, IF=2.624)
Lv Chengkun,Wang Ziao*, Dai Lei, Liu Hao, Chang Juntao, Yu Daren. Control oriented modeling for nonlinear MIMO turbofan engine based on equilibrium manifold expansion model[J]. Energies, 2021, 14(9): 6277. (SCI收录, DOI: 10.3390/en14196277, IF=3.252)
Wu Guangwei, Wang Ziao*, Shi Teng, Zhang Zhibin, Jiang Weiyu, Quan Fuxu, Chang Juntao. Effect of expansion waves on cowl shockwave and boundary layer interaction in hypersonic inlet[J]. Propulsion and Power Research, accepted.
其他作者SCI论文
Kong Chen,Wang Ziao, Zhang Junlong, Wang Xuan, Wang Kai, Li Yunfei, Chang Juntao*. Research on flame prediction in a scramjet combustor using data-driven model[J]. Physics of Fluids, 2022, 34: 066101. (SCI收录, DOI: 10.1063/5.0097631, IF=4.980)
Li Yunfei, Chang Juntao*,Wang Ziao, Kong Cheng. Inversion and reconstruction of supersonic cascade passage flow field based on a model comprising transposed network and residual network[J]. Physics of Fluids, 2019, 31: 126102. (SCI收录, DOI: 10.1063/1.5124133, IF=4.980)
Zhang Junlong, Chang Juntao*,Wang Ziao, Gao Lin, Bao Wen. Flame propagation and flashback characteristics in a kerosene fueled supersonic combustor equipped with strut/wall combined fuel injectors[J]. Aerospace Science and Technology, 2019, 93: 105303. (SCI收录, DOI: 10.1016/j.ast.2019.105303, IF=5.457)
Hou Wenxin, Chang Juntao*,Wang Ziao, Wang Youyin, Bao Wen. Shock train behavior affected by continuous Mach number variation of incoming flow[J]. Acta Astronautica, 2020, 177: 652-665. (SCI收录, DOI: 10.1016/j.actaastro.2020.08.014, IF=2.954)
Li Yunfei, Chang Juntao*, Wang Ziao, Kong Chen. An efficient deep learning framework to reconstruct the flow field sequences of the supersonic cascade channel[J]. Physics of Fluids, 2021, 33: 056106. (SCI收录, DOI: 10.1063/5.0048170, IF=4.980)
Kong Chen, Chang Juntao*, Wang Ziao, Li Yunfei. Prediction model of flow field in an isolator over various operating conditions[J]. Aerospace Science and Technology, 2021, 111: 106576. (SCI收录, DOI: 10.1016/j.ast.2021.106576, IF=5.457)
Kong Chen, Chang Juntao*,Wang Ziao, Li Yunfei, Bao Wen. Data-driven super-resolution reconstruction of supersonic flow field by convolutional neural networks[J]. AIP Advances, 2021, 11: 065321. (SCI收录, DOI: 10.1063/5.0056569, IF=1.697)
Li Yunfei, Chang Juntao*, Kong Chen,Wang Ziao. Flow field reconstruction and prediction of the supersonic cascade channel based on a symmetry neural network under complex and variable conditions[J]. AIP Advances, 2020, 10: 065116. (SCI收录, DOI: 10.1063/5.0008889, IF=1.697)
Kong Chen, Chang Juntao*, Li Yunfei, Wang Ziao. A deep learning approach for the velocity field prediction in a scramjet isolator[J]. Physics of Fluids, 2021, 33: 026103. (SCI收录, DOI: 10.1063/5.0039537, IF=4.980)
Lv Chengkun, Huang Qian, Chang Juntao*,Wang Ziao, Zheng Jialin, Yu Daren. Mode transition path optimization for turbine-based combined-cycle ramjet stage under uncertainty propagation of integrated airframe-propulsion system[J]. Energy, 2023, 268: 126718. (SCI收录, DOI: 10.1016/j.energy.2023.126718, IF=8.857)
Shi Wen, Chang Juntao*, Zhang Junlong, Ma Jicheng, Wang Ziao, Bao Wen. Numerical investigation on the forced oscillation of shock train in hypersonic inlet with translating cowl[J]. Aerospace Science and Technology, 2019, 87: 311-322. (SCI收录, DOI: 10.1016/j.ast.2019.02.022, IF=5.457)
Wang Bo, Jiang Zixiao*, Cheng Dawei,Wang Ziao. Exploring public attention and sentiment toward carbon neutrality: evidence from Chinese social media Sina Weibo[J]. Frontiers in Psychology, 2023, 14: 1200824. (SSCI收录, DOI: 10.3389/fpsyg.2023.1200824, IF=3.8)
中文论文
王子傲, 常军涛. 不同节流比下的超声速叶栅波系振荡模式及特性[J]. 工程热物理学报, 2020, 41(11): 2695-2703. (EI收录, 文章编号: 0253-231X(2020)11-2695-09)
王子傲, 陈若愚, 李一鸣, 常军涛. 超声速内流激波串流场特性及控制方法研究进展[J]. 工程热物理学报, 2022, 43(5): 1-17. (EI收录, 文章编号: 0253-231X(2022)05-0000-17)
王子傲, 黄仁哲, 信宣安, 常军涛. 来流Mach数连续变化下的激波串运动特性[J]. 气体物理, 2023, 8(02): 15-23. (DOI: 10.19527/j.cnki.2096-1642.1007)
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