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| 高超声速 V 型前缘气动特性及流场作用机理研究 学位论文 硕士论文,北京: 中国科学院大学, 2022 Authors: 姜文清![](/image/person.jpg)
Adobe PDF(4250Kb)  |   Favorite  |  View/Download:277/4  |  Submit date:2022/07/08 高超声速 V 形前缘 激波干扰 真实气体效应 |
| 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)![](/image/person.jpg)
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| 循环神经网络在智能天平研究中的应用 期刊论文 力学学报, 2021, 卷号: 53, 期号: 08, 页码: 2336-2344 Authors: 聂少军 ; 王粤 ; 汪运鹏 ; 赵敏; 隋婧
Adobe PDF(6901Kb)  |   Favorite  |  View/Download:249/65  |  Submit date:2021/11/12 气动力测量 风洞天平 动态校准 人工智能 循环神经网络 |
| 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)![](/image/person.jpg)
Adobe PDF(1129Kb)  |   Favorite  |  View/Download:364/179  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 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)![](/image/person.jpg)
Adobe PDF(2149Kb)  |   Favorite  |  View/Download:217/66  |  Submit date:2020/12/28 artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Impulse force-measurement system 期刊论文 SHOCK WAVES, 2020, 页码: 11 Authors: Wang YP(汪运鹏) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(1551Kb)  |   Favorite  |  View/Download:292/88  |  Submit date:2020/11/30 Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| 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)![](/image/person.jpg)
Adobe PDF(1090Kb)  |   Favorite  |  View/Download:289/102  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Performance and Modeling of a Two-Stage Light Gas Gun Driven by Gaseous Detonation 期刊论文 APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 12, 页码: 16 Authors: Tang WQ(唐伟奇); Wang Q(汪球) ; Wei BC(魏炳忱) ; Li JW(栗继伟); Li JP(李进平) ; Shang JH(尚甲豪); Zhang K(张坤) ; Zhao W(赵伟)![](/image/person.jpg)
Adobe PDF(6798Kb)  |   Favorite  |  View/Download:312/68  |  Submit date:2020/08/26 two-stage light gas gun detonation quasi-one-dimensional piston projectile |
| Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文 EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478 Authors: Luo ZT(罗长童) ; Wang YP(汪运鹏) ; Hu ZM(胡宗民) ; Li JP(李进平) ; Jiang ZL(姜宗林)![](/image/person.jpg)
View  |   Adobe PDF(2227Kb)  |   Favorite  |  View/Download:298/71  |  Submit date:2019/10/21 Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷) ; Chang XY(张新宇)
View  |   Adobe PDF(3918Kb)  |   Favorite  |  View/Download:558/183  |  Submit date:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |