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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
作者:  Qi L(齐力);  Han GL(韩桂来);  Jiang ZL(姜宗林)
收藏  |  浏览/下载:78/0  |  提交时间: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
作者:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:145/39  |  提交时间: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
作者:  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)  |  收藏  |  浏览/下载:55/25  |  提交时间: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
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:83/33  |  提交时间: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
作者:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Li XD(李旭东);  Shi CM(师曾敏)
浏览  |  Adobe PDF(376Kb)  |  收藏  |  浏览/下载:339/63  |  提交时间: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
作者:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载:387/68  |  提交时间: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
作者:  Li XD(李馨东);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1140Kb)  |  收藏  |  浏览/下载:451/155  |  提交时间: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
作者:  李康;  李进平;  姜宗林
浏览  |  Adobe PDF(1471Kb)  |  收藏  |  浏览/下载:368/102  |  提交时间: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
作者:  李康;  胡宗民;  姜宗林
Adobe PDF(379Kb)  |  收藏  |  浏览/下载:532/178  |  提交时间: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
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:613/137  |  提交时间:2015/03/02
Keywords: Mach Number Independence  Oswatitsch  Nonequilibrium Flow  Real-gas Effect  Expansion Effect