Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement von Wang, Youyin, Cheng, Kunlin, Tang, Jingfeng, Liu, Xiaoyong, Bao, Wen

Volltext

Chiller Fault Diagnosis Based on Automatic Machine Learning von Tian, Chongyi, Wang, Youyin, Ma, Xin, Chen, Zhuolun, Xue, Huiyu

Volltext

Feasibility and Performance Analysis of High-Energy-Density Hydrocarbon-Fueled Turboexpander Engine von Gao, Jin, Kang, Ziyi, Sun, Weiheng, Wang, Youyin, Zhang, Junlong, Bao, Wen

Volltext

Contrasting Characteristics of Atmospheric Pressure Cold Plasma Jets With Different Tube Materials von Song, Jian, Tang, Jingfeng, Wei, Liqiu, Zhang, Nan, Qian, Junjie, Wang, Youyin, Yu, Daren

Volltext

Interruption in Propagation of an Ar Atmospheric Pressure Plasma Jet Surrounded With Distilled Water von Song, Jian, Tang, Jingfeng, Wang, Youyin, Wei, Liqiu, Piao, Yongjun, Wang, Yue, Yu, Daren

Volltext

Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut von Zhang, Junlong, Chang, Juntao, Ma, Jicheng, Wang, Youyin, Bao, Wen

Volltext

Experimental study on the forced oscillation of shock train in an isolator with background waves von Hou, Wenxin, Chang, Juntao, Wang, Youyin, Kong, Chen, Bao, Wen

Volltext

Shock train behavior affected by continuous Mach number variation of incoming flow von Hou, Wenxin, Chang, Juntao, Wang, Ziao, Wang, Youyin, Bao, Wen

Volltext

Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor von Lv, Chengkun, Xu, Haiqi, Chang, Juntao, Wang, Youyin, Chen, Ruoyu, Yu, Daren

Volltext

Influence of water injection on performance of scramjet engine von Xiong, Yuefei, Qin, Jiang, Cheng, Kunlin, Wang, Youyin

Volltext

Research on the operating boundary of the dual mode scramjet with a constant area combustor through thermodynamic cycle analysis von Wang, Youyin, Hou, Wenxin, Zhang, Junlong, Tang, Jingfeng, Chang, Juntao, Bao, Wen

Volltext

Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor von Zhang, Chenlin, Chang, Juntao, Zhang, Yuanshi, Wang, Youyin, Bao, Wen

Volltext

Thermodynamic analysis of the hydrocarbon-fuelled air-turborocket engine with complete-combustion gas generator von Gao, Jin, Sun, Weiheng, Kang, Ziyi, Wang, Youyin, Zhang, Junlong, Bao, Wen

Volltext

Buzz evolution process investigation of a two-ramp inlet with translating cowl von Shi, Wen, Chang, Juntao, Wang, Youyin, Bao, Wen, Liu, Xiaoyong

Volltext

Behavior and flow mechanism of shock train self-excited oscillation influenced by background waves von Hou, Wenxin, Chang, Juntao, Xie, Zongqi, Wang, Youyin, Wu, Linke, Bao, Wen

Volltext

Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor von Feng, Shuo, Chang, Juntao, Zhang, Chenlin, Wang, Youyin, Ma, Jicheng, Bao, Wen

Volltext

Aerodynamic performance enhancement of a variable-geometry dual-mode combustor designed by the method of characteristics von Wang, Youyin, Shi, Wen, Wang, Xuan, Zhang, Junlong, Gao, Jin, Tang, Jingfeng, Chang, Juntao, Bao, Wen

Volltext

Path dependence characteristic of shock train in a 2D hypersonic inlet with variable background waves von Shi, Wen, Chang, Juntao, Ma, JiCheng, Wang, Youyin, Gao, Lin, Bao, Wen

Volltext

Numerical studies for performance improvement of a variable geometry dual mode combustor by optimizing deflection angle von Feng, Shuo, Chang, Juntao, Zhang, Yuanshi, Zhang, Chenlin, Wang, Youyin, Bao, Wen

Volltext

Numerical investigation on behaviors of shock train in a hypersonic inlet with translating cowl von Shi, Wen, Chang, Juntao, Zhang, Junlong, Wang, Youyin, Hou, Wenxin, Bao, Wen

Volltext