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| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 Authors: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  Favorite  |  View/Download:351/66  |  Submit date:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |
| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文 Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9707Kb)  |  Favorite  |  View/Download:276/78  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 Authors: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  Favorite  |  View/Download:95/2  |  Submit date:2023/03/23 |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  Favorite  |  View/Download:269/49  |  Submit date:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:167/48  |  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) Adobe PDF(1551Kb)  |  Favorite  |  View/Download:225/60  |  Submit date:2020/11/30 Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| 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) View  |  Adobe PDF(2227Kb)  |  Favorite  |  View/Download:242/56  |  Submit date:2019/10/21 Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| Experimental investigation of liquid film cooling in hypersonic flow 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10 Authors: Yuan CK(苑朝凯); Li JP(李进平); Jiang ZL(姜宗林); Yu HR(俞鸿儒) View  |  Adobe PDF(4383Kb)  |  Favorite  |  View/Download:430/123  |  Submit date:2019/06/10 |
| A Multi-space Interrelation Theory for Correlating Aerodynamic Data from Hypersonic Ground Testing 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 Authors: Jiang ZL(姜宗林); Luo ZT(罗长童) View  |  Adobe PDF(377Kb)  |  Favorite  |  View/Download:131/27  |  Submit date:2020/01/06 |
| 高超声速条件下溢流液膜厚度测量方法 期刊论文 中国科学. 技术科学, 2018, 卷号: 48, 期号: 6, 页码: 629-638 Authors: 苑朝凯; 李进平; 陈宏; 姜宗林; 俞鸿儒 View  |  Adobe PDF(4824Kb)  |  Favorite  |  View/Download:474/90  |  Submit date:2018/10/24 高超声速热防护 主动冷却 液膜厚度 电导法 |