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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：363/69 | 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 |
| 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：104/2 | 提交时间：2023/03/23 |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(3599Kb) | 收藏 | 浏览/下载：327/89 | 提交时间：2021/03/03
Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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 |
| 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 |
| AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林); Teng HH(滕宏辉)
浏览 | Adobe PDF(4139Kb) | 收藏 | 浏览/下载：271/57 | 提交时间：2019/04/19 |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
浏览 | Adobe PDF(679Kb) | 收藏 | 浏览/下载：386/68 | 提交时间：2018/01/16
Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| Development and calibration of detonation-driven high-enthalpy and hypersonic test facilities 图书章节
2016
作者: Jiang ZL(姜宗林); Yu HR(俞鸿儒)
浏览 | Adobe PDF(883Kb) | 收藏 | 浏览/下载：222/38 | 提交时间：2018/11/06 |
| A reconstructed discontinuous Galerkin method based on a Hierarchical WENO reconstruction for compressible flows on tetrahedral grids 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 236, 页码: 477-492
作者: Luo H; Xia YD; Spiegel S; Nourgaliev R; Jiang ZL(姜宗林); Luo, H (reprint author), N Carolina State Univ, Dept Mech & Aerosp Engn, Raleigh, NC 27695 USA.
Adobe PDF(2739Kb) | 收藏 | 浏览/下载：1362/496 | 提交时间：2013/03/25
Discontinuous Galerkin Method Weno Reconstruction Unstructured Grids |
