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Properties of the compressibility and transport motion in wall-bounded turbulent flows at Mach 8 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2022, 卷号: 33, 期号: 7, 页码: 2250090
作者:  Li, Xin;  Zhang, Siyuan;  Duan JY(段俊亦);  Liu, Xiaobo;  Wu, Wanghao
Adobe PDF(1752Kb)  |  收藏  |  浏览/下载：87/26  |  提交时间：2022/10/23
Direct numerical simulation  turbulent boundary layer  wall temperature effect  high Mach number  
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：328/46  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：434/214  |  提交时间：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
基于预处理HLLEW格式的全速域数值算法 期刊论文
计算物理, 2016, 卷号: 33, 期号: 3, 页码: 273-282
作者:  刘中玉;  张明锋;  郑冠男;  杨国伟
浏览  |  Adobe PDF(1164Kb)  |  收藏  |  浏览/下载：321/82  |  提交时间：2016/12/16
Preconditioning  Flow At All Mach Number  Incompressible Flow  Hllew Scheme  Implicit Time-marching  
Concept of non-ablative thermal protection system for hypersonic vehicles 期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
作者:  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)  |  收藏  |  浏览/下载：1375/490  |  提交时间：2013/04/07
Flow Fields  Flow Visualization  Hypersonic Aerodynamics  Hypersonic Vehicles  Mach Number  Shock Waves  Thermal Insulating Materials  Engineering Applications  Experimental Datum  Hypersonic Wind Tunnels  Numerical Results  Stagnation Points  Thermal Protection  Thermal Protection System  Working Pressures  
The applicability of Mach number independence principle in case of hypersonic thermo-chemical nonequilibrium flow 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012
作者:  Li K(李康);  Li JP(李进平);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1755Kb)  |  收藏  |  浏览/下载：608/136  |  提交时间：2015/03/02
Keywords: Mach Number Independence  Oswatitsch  Nonequilibrium Flow  Real-gas Effect  Expansion Effect  
Low diffusion E-CUSP scheme with implicit high order WENO scheme for preconditioned Navier-Stokes equations 期刊论文
COMPUTERS & FLUIDS, 2012, 卷号: 55, 页码: 13-23
作者:  Shen YQ(申义庆);  Zha GC;  Zha, GC;  Univ Miami, Dept Mech & Aerosp Engn, Coral Gables, FL 33124 USA.
Adobe PDF(3419Kb)  |  收藏  |  浏览/下载：1057/333  |  提交时间：2013/01/18
Preconditioing  Weno Scheme  All Flow Speeds  Incompressible Flows  Compressible Flows  Flux-splitting Methods  Upwind Scheme  Compressible Flows  Mach-number  Viscous Flows  Computation  Accurate  Simulations  Sequel  Speeds