|
Selected(0)Clear
Items/Page: Sort: |
| 高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors: 汪运鹏 ; 姜宗林
 Adobe PDF(2086Kb) |  Favorite | View/Download：255/75 | Submit date：2021/01/29 |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
 Adobe PDF(1129Kb) | Favorite | View/Download：361/179 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Specific signal imaging velocimetry for rarefied plasma flows 期刊论文
EXPERIMENTS IN FLUIDS, 2020, 卷号: 61, 期号: 12, 页码: 247
Authors: Cao JW(曹进文); Huang HJ(黄河激); Pan WX(潘文霞); Meng X(孟显); Wu CK(吴承康)
Adobe PDF(4736Kb) | Favorite | View/Download：300/89 | Submit date：2020/12/28
MOLECULAR TAGGING VELOCIMETRY MACH PROBE VELOCITY TURBULENT JETS |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2149Kb) | Favorite | View/Download：212/63 | Submit date：2020/12/28
artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | Favorite | View/Download：364/112 | Submit date：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| Coaxial Thermocouples for Heat Transfer Measurements in Long-Duration High Enthalpy Flows 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 18, 页码: 18
Authors: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)
Adobe PDF(7131Kb) | Favorite | View/Download：328/97 | Submit date：2020/11/30
heat transfer measurement coaxial thermocouple long-duration semi-infinite high enthalpy |
| Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors: Xue R; Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
Adobe PDF(3912Kb) | Favorite | View/Download：363/242 | Submit date：2020/08/26
Compressible boundary layer combustion Skin-friction reduction Boundary layer transition Transition k-kl-w model Hydrogen combustion |
| 基于深度学习技术的激波风洞智能测力系统研究 期刊论文
力学学报, 2020, 卷号: 52, 期号: 05, 页码: 1304-1313
Authors: 汪运鹏; 杨瑞鑫; 聂少军; 姜宗林
Adobe PDF(1037Kb) | Favorite | View/Download：261/73 | Submit date：2020/11/18
激波风洞 人工智能 测力系统 动态校准 气动力测量 应变天平 |
| Evaluation of Actuator Disk Model Relative to Actuator Surface Model for Predicting Utility-Scale Wind Turbine Wakes 期刊论文
ENERGIES, 2020, 卷号: 13, 期号: 14, 页码: 18
Authors: Li ZB(李曌斌); Yang XL(杨晓雷)
Adobe PDF(9697Kb) | Favorite | View/Download：280/99 | Submit date：2020/09/07
wind turbine wake actuator disk model actuator surface model dynamic mode decomposition coherent structures wake meandering |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
Adobe PDF(1090Kb) | Favorite | View/Download：285/102 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
