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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:361/69  |  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 |
| 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:287/82  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27 作者: Li, Mengzhe; Wang, Zhikai; Xu, Rongguang; Zhang, Xiaoliang; Chen, Zhitong; Wang Q(汪球) Adobe PDF(8841Kb)  |  收藏  |  浏览/下载:263/105  |  提交时间:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| Characteristics of wall-shear stress fluctuations in shock wave and turbulent boundary layer interaction 期刊论文 JOURNAL OF TURBULENCE, 2021, 页码: 23 作者: Tong FL(童福林); Duan JY(段俊亦); Li XL(李新亮) Adobe PDF(5190Kb)  |  收藏  |  浏览/下载:230/60  |  提交时间:2021/11/01 Wall-shear stress shock wave turbulent boundary layers |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:374/56  |  提交时间: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 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:313/165  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:261/107  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文 ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23 作者: Xue R; Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C Adobe PDF(3912Kb)  |  收藏  |  浏览/下载:325/222  |  提交时间:2020/08/26 Compressible boundary layer combustion Skin-friction reduction Boundary layer transition Transition k-kl-w model Hydrogen combustion |
| Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner 期刊论文 JOURNAL OF TURBULENCE, 2020, 页码: 20 作者: Tong FL(童福林); Chen JQ; Sun D; Li XL(李新亮) Adobe PDF(5228Kb)  |  收藏  |  浏览/下载:190/82  |  提交时间:2020/08/26 Wall-shear stress expansion corner supersonic turbulent boundary layer direct numerical simulation |
| Modeling De-NOx by Injection Ammonia in High Temperature Zone of Cement Precalciner 期刊论文 JOURNAL OF THERMAL SCIENCE, 2020 作者: Zhang LY(张乐宇); Wei XL(魏小林); Zhang ZX; Li S(李森) Adobe PDF(1220Kb)  |  收藏  |  浏览/下载:263/137  |  提交时间:2020/12/28 cement precalciner SELECTIVE NONCATALYTIC REDUCTION coal combustion NUMERICAL-SIMULATION CaCO3 decomposition SNCR high temperature zone COMBUSTION SNCR OPTIMIZATION |