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Transient buildup and dissipation of a compressed plasma shockwave in arc-discharge plasma beams 期刊论文
Plasma Sources Science and Technology, 2021, 卷号: 30, 期号: 12, 页码: 15
作者:  Zhang,Zhe;  Fu,Yifeng;  Zhang,Zun;  Lin X(林鑫);  Qi,Jiayun;  Ling,William Yeong Liang;  Tang,Haibin;  Herdrich,Georg
Adobe PDF(3997Kb)  |  收藏  |  浏览/下载：272/74  |  提交时间：2022/01/24
electric propulsion  plasma shockwave  ultra-high speed imaging  plasma compression  
高压捕获翼构型亚跨超流动特性数值研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 11, 页码: 3056-3070
作者:  王浩祥;  李广利;  杨靖;  肖尧;  王小永;  徐应洲;  许先贵;  崔凯
Adobe PDF(2607Kb)  |  收藏  |  浏览/下载：280/69  |  提交时间：2022/03/16
高压捕获翼  计算流体力学  宽速域  流动分离  气动干扰  
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
作者:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  收藏  |  浏览/下载：316/56  |  提交时间：2022/01/12
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV 期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
作者:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平);  Tong FL(童福林)
Adobe PDF(4454Kb)  |  收藏  |  浏览/下载：272/34  |  提交时间：2021/11/01
Lifting body model  Hypersonic transition  Direct numerical simulation  
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：270/57  |  提交时间：2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit  
A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15
作者:  Zhao, Cheng;  Yang Y(杨焱);  Zhang, Tao;  Dong, Haibo;  Hou, Guoxiang
Adobe PDF(3919Kb)  |  收藏  |  浏览/下载：315/76  |  提交时间：2021/08/30
Acoustic perturbation equations  Immersed boundary method  Flow-induced noise  Four-cylinder array  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  收藏  |  浏览/下载：337/49  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider 期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
作者:  刘文;  张陈安;  Wang Xiao-Peng;  Li Jin-Jie;  王发民
Adobe PDF(7528Kb)  |  收藏  |  浏览/下载：367/56  |  提交时间：2021/08/30
Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
作者:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯)
Adobe PDF(1179Kb)  |  收藏  |  浏览/下载：229/97  |  提交时间：2021/06/11
bluntness method  computational fluid dynamics  hypersonic  volume  Waverider  
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
作者:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  收藏  |  浏览/下载：339/95  |  提交时间：2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection