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Differences in Performance of Models for Heterogeneous Cores during Pulse Decay Tests 期刊论文
APPLIED SCIENCES-BASEL, 2019, 卷号: 9, 期号: 15, 页码: 21
作者:  Han GF(韩国锋);  Chen, Y;  Liu, M;  Liu, XL
浏览  |  Adobe PDF(7403Kb)  |  收藏  |  浏览/下载：222/52  |  提交时间：2019/10/21
pulse decay test  dual-porosity model  dual-permeability model  pseudo-state interporosity flow  transient interporosity flow  
Deformation behavior of non-rigid airships in wind tunnel tests 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 3, 页码: 611-618
作者:  Lu LL(路玲玲);  Song HW(宋宏伟);  Wang YW(王一伟);  Huang CG(黄晨光)
浏览  |  Adobe PDF(3480Kb)  |  收藏  |  浏览/下载：398/66  |  提交时间：2019/01/09
Angle of attack  Fiber Bragg grating sensor  Flow velocity  Internal pressure  Non-rigid airship  Wind tunnel test  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
作者:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(532Kb)  |  收藏  |  浏览/下载：627/151  |  提交时间：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
作者:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
浏览  |  Adobe PDF(1617Kb)  |  收藏  |  浏览/下载：1564/914  |  提交时间：2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
Monte Carlo modeling of electron density in hypersonic rarefied gas flows 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18, 2014
作者:  Fan J(樊菁);  Zhang YH(张羽淮);  Jiang JZ(蒋建政)
浏览  |  Adobe PDF(835Kb)  |  收藏  |  浏览/下载：661/175  |  提交时间：2015/01/21
Hypersonic Rarefied Gas Flow  Electron Density  Dsmc  Tss  Ram-c Ii Flight Test  
Uniaxial tensile and cross-sectional indentation tests to investigate the adhesion between the brittle Cr coating and the ductile steel substrate 会议论文
2011 1st International Conference on Mechanical Engineering, ICME 2011, Phuket, Thailand, APR 03-04, 2011
作者:  Yang BQ(杨班权);  Chen GN(陈光南);  Chen XJ(陈学军);  Yang BQ(杨班权)
Adobe PDF(246Kb)  |  收藏  |  浏览/下载：769/112  |  提交时间：2013/02/26
Adhesion  Carbon Steel  Mechanical Engineering  Shear Flow  Shear Strength  Substrates  Tensile Strength  Tensile Testing  Testing  Coating-substrate Systems  Cr Coating  Cross-sectional Indentations  Crucial Parameters  Ductile Steel Substrate  Flow Stress  Interfacial Decohesion  Lower Bounds  Maximum Shears  Normal Medium Carbon Steel  Ultimate Shear Strength  Uniaxial Tensile Test  
Ductile To Brittle Transition In Dynamic Fracture Of Brittle Bulk Metallic Glass 期刊论文
Journal of Applied Physics, 2008
作者:  Wang G;  Han YN;  Xu XH(许向红);  Ke FJ(柯孚久);  Han BS;  Wang WH;  Wang, WH (reprint author), Chinese Acad Sci, Inst Phys, POB 603, Beijing 100080, Peoples R China.
Adobe PDF(452Kb)  |  收藏  |  浏览/下载：825/232  |  提交时间：2009/08/03
Test Temperature  Behavior  Deformation  Toughness  Mechanism  Niobium  Alloy  State  Flow  
Flow Mechanism of Polymer Solution in Porous Media and in Situ Test Data Analysis 期刊论文
JOURNAL OF CENTRAL SOUTH UNIVERSITY OF TECHNOLOGY, 2007, 卷号: 14, 页码: 54-58
作者:  Liu YW(刘曰武);  Liu, YW (reprint author), Chinese Acad Sci, Inst Mech, Div Engn Sci, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(458Kb)  |  收藏  |  浏览/下载：172/78  |  提交时间：2016/01/11
Polymer Solution  Numerical Simulation  Transient Flow  Test Data  Power Law Index  
Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
作者:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(4312Kb)  |  收藏  |  浏览/下载：146/62  |  提交时间：2017/06/01
Compressible Navier-stokes  Computational Studies  Experimental Comparison  Experimental Investigations  Flow Charac-teristics  Hypersonic Propulsion Test Facility  Performance Parameters  Scramjet Inlets  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：213/80  |  提交时间：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures