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Space advanced technology demonstration satellite 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 页码: 19./通讯作者：Zhang, Xiaofeng, Zhang, Yonghe
Authors:  Zhang, Xiaofeng;  Chen, Wen;  Zhu, Xiaocheng;  Meng, Na;  He, Junwang;  Bi, Xingzi;  Zhang, Yonghe;  Shi, Qi;  Li, Fei;  Liu, Rui;  Feng, Zhenggong;  Liu, Liu;  Li, Jinsong;  Wu, Haichen;  Xu, Dongxiao;  Li, Taijie;  Huang, Jiangjiang;  Liu, Shuo;  Li, Tiantong;  Yu, Xiansheng;  Gao, Yang;  Zhou, Heng;  Ban, Hanyu;  Zhang, Yanli;  Zhang, Yueting;  Yang, Yingquan;  He, Tao;  Duan, Xuliang;  Chen, Xin;  Wang, Yamin;  Sun, Antai;  Zhang, Kuoxiang;  Sun, Ying;  Wang, Yaobin;  Fan, Chengcheng;  Xiong, Shaolin;  Li, Xinqiao;  Wen, Xiangyang;  Ling, Zhixing;  Sun, Xiaojin;  Zhang, Chen;  Bai, Xianyong;  Wang, Zhanshan;  Deng, Yuanyong;  Tian, Hui;  Yang, Jianfeng;  Xue, Hongbo;  Sang, Peng;  Liu, Jinguo;  Zheng, Huilong;  Zhu, Xiang;  He JW(贺建武);  Li, Hui;  Xu, Luxiang;  Xu, Shuyan;  Chen, Wenwu;  Liu, Zhendong;  Wang, Zhaoli;  Mao, Xianglong;  Gao, Rong;  Li, Zongxuan;  Ding, Guopeng;  Wang, Xinyu;  Dou, Runjiang;  Weng, Lubin;  Luo, Hao;  Wang, Yaping;  Liang, Xianfeng;  Fang, Ziruo
Adobe PDF(5267Kb)  |  Favorite  |  View/Download：223/63  |  Submit date：2024/02/05
SATech-01  spacecraft design  scientific instruments  on-orbit performance  
Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295./通讯作者：Wu, K
Authors:  Ao Y(敖彧);  Wu K(吴坤);  Lu, Hongbo;  Ji, Feng;  Fan XJ(范学军)
Adobe PDF(11339Kb)  |  Favorite  |  View/Download：331/15  |  Submit date：2023/06/15
Hypervelocity combustion  Thermal nonequilibrium  Two-temperature model  Numerical simulation  
Role of wall temperature on shock train in a rectangular isolator 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:  Lu HB;  Wang D;  Chen X;  Yue LJ(岳连捷);  Ji, Feng ([email protected])
View  |  Adobe PDF(560Kb)  |  Favorite  |  View/Download：332/116  |  Submit date：2017/05/05
Aero  Heating  Dual Mechanisms  On Flow  Shock Train  Specific Heat Ratio  Total Pressure  Total Temperatures  Wall Temperatures