中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共29条，第1-10条 帮助

限定条件                        
已选(0)清除 条数/页：   排序方式：
Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
作者:  Chang SY(常思源);  Xiao Y(肖尧);  Li GL(李广利);  Tian ZW(田中伟);  Cui K(崔凯)
收藏  |  浏览/下载：85/0  |  提交时间：2024/01/22
High-pressure capturing wing  Subsonic  Numerical simulation  Wing dihedral  Stability  
Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15
作者:  Chang SY(常思源);  Xiao Y(肖尧);  Li GL(李广利);  Tian ZW(田中伟);  Cui K(崔凯)
Adobe PDF(8136Kb)  |  收藏  |  浏览/下载：57/7  |  提交时间：2024/03/11
High-pressure capturing wing  Hypersonic  Numerical simulation  Wing dihedral  Stability  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
作者:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  收藏  |  浏览/下载：106/24  |  提交时间：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
On jet-wake flame stabilization in scramjet: A LES/RANS study from chemical kinetic and fluid-dynamical perspectives 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 120, 页码: 12
作者:  Wu K(吴坤);  Zhang, Peng;  Fan XJ(范学军)
Adobe PDF(3834Kb)  |  收藏  |  浏览/下载：325/51  |  提交时间：2022/01/24
Supersonic combustion  Jet-wake flame stabilization  Hybrid LES  RANS  Detailed hydrogen chemistry  Counter-rotating vortex pair  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  收藏  |  浏览/下载：275/108  |  提交时间：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
作者:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  收藏  |  浏览/下载：281/64  |  提交时间：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
作者:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  收藏  |  浏览/下载：269/57  |  提交时间：2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  收藏  |  浏览/下载：133/46  |  提交时间：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
作者:  Wang KL(王宽亮);  Yang PF(杨鹏飞);  Teng HH(滕宏辉)
Adobe PDF(2853Kb)  |  收藏  |  浏览/下载：244/69  |  提交时间：2021/05/17
Oblique detonation  Wave complex  Instability  Thermal choking  Expansion corner  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载：391/67  |  提交时间：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow