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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
作者:  Ao Y(敖彧);  Wu K(吴坤);  Lu, Hongbo;  Ji, Feng;  Fan XJ(范学军)
Adobe PDF(11339Kb)  |  收藏  |  浏览/下载:79/1  |  提交时间:2023/06/15
Hypervelocity combustion  Thermal nonequilibrium  Two-temperature model  Numerical simulation  
Simplified analytical models for hypersonic lateral-directional stability 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 198, 页码: 431-444
作者:  Guo SQ(郭帅旗);  Liu W(刘文);  Zhang CA(张陈安);  Zhou X(周翔);  Wang FM(王发民)
Adobe PDF(6978Kb)  |  收藏  |  浏览/下载:173/45  |  提交时间:2022/10/23
Lateral stability  Directional stability  Analytical model  Viscous effects  
Thermochemical non-equilibrium effects on hypersonic shock wave/turbulent boundary-layer interaction 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 192, 页码: 1-14
作者:  Jiang, Hao;  Liu, Jun;  Luo, Shichao;  Huang, Wei;  Wang, Junyuan;  Liu MK(刘美宽)
Adobe PDF(9113Kb)  |  收藏  |  浏览/下载:224/35  |  提交时间:2022/05/17
Hypersonic flow  Shock wave/turbulent boundary-layer interactions  Thermochemical non-equilibrium  Turbulence model  
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
作者:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  收藏  |  浏览/下载:332/226  |  提交时间:2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion