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| Numerical Simulation Research on Thermal Response Characteristics of E-type Coaxial Thermocouples 会议论文
2021 2rd International Conference on Applied Mechanics and Mechanical Engineering, 长沙, 2021/09/12
Authors: Qi L(齐力) ; Han GL(韩桂来); Jiang ZL(姜宗林)
  Favorite | View/Download：83/0 | Submit date：2022/07/06
气动热 同轴热电偶 数值模拟 |
| A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安，中国, 19-21 December 2020
Authors: Chen Z(陈阵); Li S(李森); Luo ZT(罗长童); Jiang ZL(姜宗林)
 Adobe PDF(1545Kb) | Favorite | View/Download：156/42 | Submit date：2021/02/01 |
| Influence of Dual Ignition on Test Conditions of a High-Enthalpy Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Wang Q(汪球); Zhao W(赵伟); Li JW(栗继伟); Li JP(李进平); Lu P(卢盼); Jiang ZL(姜宗林)
Adobe PDF(240Kb) | Favorite | View/Download：66/27 | Submit date：2023/03/17 |
| 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
Authors: 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) | Favorite | View/Download：97/36 | Submit date：2023/03/17 |
| The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Wang C(王春); Xiang GX(项高翔); Jiang ZL(姜宗林); Li XD(李旭东); Shi CM(师曾敏)
 View | Adobe PDF(376Kb) | Favorite | View/Download：353/66 | Submit date：2020/01/06 |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
View | Adobe PDF(679Kb) | Favorite | View/Download：402/75 | Submit date：2018/01/16
Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| A New Flux Splitting Scheme for Euler Equations of Gas Dynamics 会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
Authors: Li XD(李馨东); Hu ZM(胡宗民); Jiang ZL(姜宗林)
View | Adobe PDF(1140Kb) | Favorite | View/Download：465/162 | Submit date：2015/09/29
Flux Splitting Hybrid Upwind Method Ausm Scheme K-cusp Scheme |
| 高超声速化学反应对钝体绕流流动特征的影响 会议论文
北京力学会第19届学术年会, 中国北京, 2013-01-12
Authors: 李康; 李进平; 姜宗林
View | Adobe PDF(1471Kb) | Favorite | View/Download：374/102 | Submit date：2014/04/02
化学反应 钝体绕流 流动特征 高温气体动力学 高超声速流动 激波形状 壁面 理论分析 速度分布 热化学非平衡 流线 能量分配 组分浓度 无粘流动 数值模拟分析 参数分布 数值方法 组分变化 边界层 量热 |
| 混合格式在高超声速气动热模拟中的特性研究 会议论文
LHD2013夏季学术研讨会, 河北平山, 2013
Authors: 李康; 胡宗民; 姜宗林
Adobe PDF(379Kb) | Favorite | View/Download：541/182 | Submit date：2014/01/23
高超声速流动 钝头体 混合格式 气动热 数值特性 |
| 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
Authors: Li K(李康); Li JP(李进平); Jiang ZL(姜宗林)
Adobe PDF(1755Kb) | Favorite | View/Download：627/142 | Submit date：2015/03/02
Keywords: Mach Number Independence Oswatitsch Nonequilibrium Flow Real-gas Effect Expansion Effect |
