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| Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53 Authors: Nie SJ(聂少军); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2346Kb)  |  Favorite  |  View/Download:80/17  |  Submit date:2024/02/26 Convolutional neural net-works Deep learning Frequency domain analysis Force measurement Time domain analysis Recurrent neural networks |
| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文 NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19 Authors: Qi L(齐力); Han GL(韩桂来); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(3726Kb)  |  Favorite  |  View/Download:303/69  |  Submit date:2022/07/18 Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| Numerical investigation on the generation mechanism of aero-heating of rudder shaft from three-dimensional flow separation and vortices 期刊论文 AIP ADVANCES, 2022, 卷号: 12, 期号: 4, 页码: 13 Authors: Lin MY(林明月); Yang F(杨帆); Wang C(王春) Adobe PDF(16512Kb)  |  Favorite  |  View/Download:196/28  |  Submit date:2022/07/18 |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  Favorite  |  View/Download:179/46  |  Submit date:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 Authors: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  Favorite  |  View/Download:350/69  |  Submit date:2022/01/12 |
| 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:357/178  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |