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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
Authors: Wang Y(王粤) ; Wang YP(汪运鹏); Jiang ZL(姜宗林)
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Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| 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
Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(9327Kb) | Favorite | View/Download：209/67 | Submit date：2023/05/26
Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文
APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11
Authors: Qi L(齐力); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(5274Kb) | Favorite | View/Download：192/7 | Submit date：2022/11/21
Coaxial thermocouples Lateral heat conduction Maximum temperature point Optimal design Numerical simulation |
| 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：396/75 | 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 |
| 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
Authors: Han GL(韩桂来); Qi L(齐力); Jiang ZL(姜宗林)
Adobe PDF(1715Kb) | Favorite | View/Download：273/42 | Submit date：2022/11/08
Heat flux Measurement Data processing Error Approximate solution |
| 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：316/93 | Submit date：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
Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2434Kb) | Favorite | View/Download：325/86 | Submit date：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 |
| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19
Authors: Qi L(齐力); Han GL(韩桂来); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林)
Adobe PDF(3726Kb) | Favorite | View/Download：266/53 | Submit date：2022/07/18
Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| 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：113/2 | Submit date：2023/03/23 |
| Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors: Zhang WS(张文硕); Zhang, Zijian; Jiang ZL(姜宗林); Han X(韩信); Liu, Yunfeng; Wang, Chun
Adobe PDF(15045Kb) | Favorite | View/Download：253/27 | Submit date：2022/01/24 |
