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| Numerical simulation of ti-based metallic glasses as whipple shield bumper by smoothed particle hydrodynamics methods 会议论文
20th Chinese Materials Conference, CMC 2019, 10 July 2019 through 14 July 2019
作者: Tang WQ(唐伟奇); Zhang K(张坤) ; Li YS(李炎森); Wang Y(王洋); Zhang YT(张亚婷); Wei BC(魏炳忱)
 Adobe PDF(1867Kb) |  收藏 | 浏览/下载：187/63 | 提交时间：2021/06/11
Hypervelocity impact Metallic glasses (MGs) Smoothed particle hydrodynamics (SPH) Whipple shield |
| Using Deep Learning Techniques for Sandwich Panels with Truss Core Damage Detection 会议论文
2019 International Conference on Advanced Electronic Materials, Computers and Materials Engineering (AEMCME 2019), Changsha, China, 19–21 April 2019
作者: Wang YB(王亚博); Lu LL(路玲玲); Song HW(宋宏伟)
Adobe PDF(1150Kb) | 收藏 | 浏览/下载：190/46 | 提交时间：2019/09/29
deep learning sandwich panels with truss core damage dection |
| Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Wang Q(汪球); Lu P(卢盼); Li JW(栗继伟); Wu S(吴松); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
Adobe PDF(299Kb) | 收藏 | 浏览/下载：84/33 | 提交时间：2023/03/17 |
| Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
作者: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH(张莫晗)
Adobe PDF(2782Kb) | 收藏 | 浏览/下载：162/62 | 提交时间：2020/11/20
Aerothermal condition Cooling effectiveness Cooling performance Thermal sensitivity Turbine vane |
| The behavior of crack initiation and early growth in high-cycle and very-high-cycle fatigue regimes for a titanium alloy 会议论文
4th IJFatigue and FFEMS Joint Workshop on Characterisation of Crack Tip Fields, Bonifacio, FRANCE, APR 10-12, 2017
作者: Pan XN(潘向南); Su H(苏杭); Sun CQ(孙成奇); Hong YS(洪友士)
 Adobe PDF(6409Kb) | 收藏 | 浏览/下载：378/61 | 提交时间：2019/04/19
Very-high-cycle fatigue Crack initiation Mean stress Titanium alloy Equiaxed microstructure |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(805Kb) | 收藏 | 浏览/下载：395/147 | 提交时间：2018/06/06 |
| On the instability of chip flow in high-speed machining 会议论文
IUTAM Symposium on Dynamic Instabilities in Solids, Madrid, SPAIN, MAY 17-20, 2016
作者: Ye GG(叶贵根); Jiang MQ(蒋敏强); Xue SF; Ma W(马维); Dai LH(戴兰宏)
 浏览 | Adobe PDF(4573Kb) | 收藏 | 浏览/下载：262/45 | 提交时间：2019/04/19
High-speed machining Shear banding Serrated chip flow Thermoplastic instability |
| MOLECULAR DYNAMICS SIMULATIONS ON THE TENSILE DEFORMATION AND FAILURE OF A POLYETHYLENE/COPPER INTERFACE 会议论文
ASME International Design Engineering Technical Conferences (IDETC) / Computers and Information in Engineering Conference (CIE), Quebec City, CANADA, AUG 26-29, 2018
作者: Liao LJ(廖丽涓); Meng CY(孟昶宇); Huang CG(黄晨光)
浏览 | Adobe PDF(1821Kb) | 收藏 | 浏览/下载：262/94 | 提交时间：2019/04/19 |
| 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：443/217 | 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 |
| Development of zone flamelet model for scramjet combustor modeling 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); Fan XJ(范学军)
浏览 | Adobe PDF(623Kb) | 收藏 | 浏览/下载：263/90 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
