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| Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
作者: Wang Y(王粤) ; Wang YP(汪运鹏); Jiang ZL(姜宗林)
 Adobe PDF(7258Kb) |  收藏 | 浏览/下载：74/15 | 提交时间：2024/01/15
Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| Numerical simulation of hypersonic flat-plate boundary-layer blowing control 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 12, 页码: 16
作者: Li ZX(李宗贤); Liu MK(刘美宽); Han GL(韩桂来); Wang DG(王大高); Jiang ZL(姜宗林)
Adobe PDF(4748Kb) | 收藏 | 浏览/下载：27/4 | 提交时间：2024/03/11 |
| Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model 期刊论文
COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6
作者: Han X(韩信); Liu YF(刘云峰); Zhang, Zijian; Zhang WS(张文硕); Yuan CK(苑朝凯); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(1092Kb) | 收藏 | 浏览/下载：70/4 | 提交时间：2023/11/28 |
| Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者: Jiang ZL(姜宗林)
Adobe PDF(10386Kb) | 收藏 | 浏览/下载：29/1 | 提交时间：2024/02/26
Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
作者: 王粤; 汪运鹏; 姜宗林
Adobe PDF(6797Kb) | 收藏 | 浏览/下载：340/35 | 提交时间：2022/12/01
两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124
作者: Wang DG(王大高); Han GL(韩桂来); Liu MK(刘美宽); Jiang ZL(姜宗林)
Adobe PDF(10056Kb) | 收藏 | 浏览/下载：48/0 | 提交时间：2023/09/26 |
| Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(9327Kb) | 收藏 | 浏览/下载：188/61 | 提交时间：2023/05/26
Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| 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 |
| 一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
作者: 王粤; 汪运鹏; 王春; 姜宗林
Adobe PDF(4901Kb) | 收藏 | 浏览/下载：561/78 | 提交时间：2022/07/11
两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
作者: Han GL(韩桂来); Qi L(齐力); Jiang ZL(姜宗林)
Adobe PDF(1715Kb) | 收藏 | 浏览/下载：252/39 | 提交时间：2022/11/08
Heat flux Measurement Data processing Error Approximate solution |
