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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties 期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
Authors:  Wang, Ruoyan;  Lin, Xin;  Wang, Zezhong;  Wu, Kun;  Pan, Junjie;  Zhang, Zelin;  Luo, Jiaxiao;  Li, Fei;  Yu, Xilong
Favorite  |  View/Download：4/0  |  Submit date：2024/05/21
Hybrid rocket  Composite fuel grain  Characteristic structure  Radiation image  Combustion properties  
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
Authors:  Ao Y(敖彧);  Wu K(吴坤);  Lu, Hongbo;  Ji, Feng;  Fan XJ(范学军)
Adobe PDF(11339Kb)  |  Favorite  |  View/Download：96/5  |  Submit date：2023/06/15
Hypervelocity combustion  Thermal nonequilibrium  Two-temperature model  Numerical simulation  
An experimental investigation of supersonic combustion of cracked JP-10 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 203, 页码: 329-340
Authors:  Cui NF(崔乃夫);  Rao W(饶威);  Li YJ(李昱君);  Zhu, Yinhai;  Zhang TC(张泰昌);  Fan XJ(范学军)
Adobe PDF(14542Kb)  |  Favorite  |  View/Download：138/5  |  Submit date：2023/02/07
Cracking  JP-10  Supersonic combustion  Regenerative cooling  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  Favorite  |  View/Download：345/234  |  Submit date：2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion