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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：367/70 | 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：298/85 | 提交时间：2022/11/14
Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2434Kb) | 收藏 | 浏览/下载：309/82 | 提交时间：2022/08/23
Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| 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
作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | 收藏 | 浏览/下载：323/169 | 提交时间：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
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2149Kb) | 收藏 | 浏览/下载：182/53 | 提交时间：2020/12/28
artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
作者: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1657Kb) | 收藏 | 浏览/下载：266/91 | 提交时间：2020/08/26
Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| 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
作者: 汪运鹏; 杨瑞鑫; 聂少军; 姜宗林
Adobe PDF(1037Kb) | 收藏 | 浏览/下载：233/69 | 提交时间：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 |
| 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：251/57 | 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：438/126 | 提交时间：2019/06/10 |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
作者: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
浏览 | Adobe PDF(1937Kb) | 收藏 | 浏览/下载：262/86 | 提交时间：2018/10/30
Hypersonic Shock tunnel Start-up process Impulse force Vibration |
