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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
作者: Wang Y(王粤) ; Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林)
 Adobe PDF(5479Kb) |  收藏 | 浏览/下载：362/69 | 提交时间：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
作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(9707Kb) | 收藏 | 浏览/下载：289/82 | 提交时间：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
作者: Jiang ZL(姜宗林); Teng, Honghui
 Adobe PDF(13641Kb) | 收藏 | 浏览/下载：101/2 | 提交时间：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
作者: 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) | 收藏 | 浏览/下载：276/53 | 提交时间：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
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2149Kb) | 收藏 | 浏览/下载：177/51 | 提交时间：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
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | 收藏 | 浏览/下载：233/63 | 提交时间：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
作者: 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)
 浏览 | Adobe PDF(2227Kb) | 收藏 | 浏览/下载：245/56 | 提交时间：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
作者: Yuan CK(苑朝凯); Li JP(李进平); Jiang ZL(姜宗林); Yu HR(俞鸿儒)
浏览 | Adobe PDF(4383Kb) | 收藏 | 浏览/下载：434/124 | 提交时间：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
作者: Jiang ZL(姜宗林); Luo ZT(罗长童)
浏览 | Adobe PDF(377Kb) | 收藏 | 浏览/下载：137/29 | 提交时间：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
作者: 苑朝凯; 李进平; 陈宏; 姜宗林; 俞鸿儒
浏览 | Adobe PDF(4824Kb) | 收藏 | 浏览/下载：497/93 | 提交时间：2018/10/24
高超声速热防护 主动冷却 液膜厚度 电导法 |
