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| 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:218/69  |  Submit date: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 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:420/79  |  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 |
| 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:329/96  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184 Authors: Teng, Honghui; Zhang, Yuhang; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(1747Kb)  |  Favorite  |  View/Download:196/40  |  Submit date:2022/07/18 Double wedge Hypersonic flow Initiation structures Oblique detonation Shock interactions |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  Favorite  |  View/Download:168/41  |  Submit date:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 7 Authors: Peng, Di; Liu, Xu; Jiao, Lingrui; Li, Ziyan; Wen, Xin; Yuan CK(苑朝凯); Han GL(韩桂来); Liu YF(刘云峰); Liu, Yingzheng; Jiang ZL(姜宗林) Adobe PDF(3477Kb)  |  Favorite  |  View/Download:277/56  |  Submit date:2021/03/30 Temperature-sensitive paint Time-resolved measurement Hypersonic flow Background radiation |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 Authors: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  Favorite  |  View/Download:414/69  |  Submit date:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| 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 Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  Favorite  |  View/Download:352/177  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247 Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(2818Kb)  |  Favorite  |  View/Download:309/118  |  Submit date:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download:420/98  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |