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| Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
作者: Peng J(彭俊); Li S(李帅) ; Yang F(杨帆); Lin MY(林明月); Han GL(韩桂来); Hu ZM(胡宗民)
 Adobe PDF(2838Kb) |  收藏 | 浏览/下载：58/1 | 提交时间：2023/04/20
Shock interactions Transitional configuration Aerodynamic heating Shear layer Mach interaction |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
作者: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮)
Adobe PDF(4402Kb) | 收藏 | 浏览/下载：194/44 | 提交时间：2021/06/07
Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| 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：380/57 | 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：321/168 | 提交时间：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
Adobe PDF(1090Kb) | 收藏 | 浏览/下载：252/101 | 提交时间：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
 浏览 | Adobe PDF(4075Kb) | 收藏 | 浏览/下载：293/85 | 提交时间：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
作者: Zhu JJ; Wang XJ; Zhang HG; Li YW; Wang RX(王睿星); Qiu ZP
浏览 | Adobe PDF(2082Kb) | 收藏 | 浏览/下载：420/189 | 提交时间：2020/03/21
Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system Uncertainty |
| Nonlinear thermo-structural behavior of sandwich panels with truss cores under through-thickness gradient temperature field 期刊论文
Theoretical and Applied Mechanics Letters, 2018, 卷号: 8, 期号: 3, 页码: 184-192
作者: 袁武,宋宏伟,黄晨光
浏览 | Adobe PDF(799Kb) | 收藏 | 浏览/下载：248/59 | 提交时间：2018/10/24
Sandwich panel with truss core Thermal protection system Thermo-structural response Nonlinear bending Post-buckling |
| Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
作者: Xiang GX(项高翔); Wang C(王春); Teng HH(腾宏辉); Jiang ZL(姜宗林)
浏览 | Adobe PDF(1161Kb) | 收藏 | 浏览/下载：301/73 | 提交时间：2018/10/30
Body And Wing Flow Field Hypersonic Flow Shock/shock Interaction Wave Configurations |
| Dynamic rupture of metal sheet subjected to laser irradiation and tangential subsonic airflow 期刊论文
Theoretical & Applied Mechanics Letters, 2018, 卷号: 8, 期号: 4, 页码: 272-276
作者: Xing XD; Ma T(马特); Wang RX(王睿星); Chao CY; Song HW(宋宏伟); Huang CG(黄晨光)
浏览 | Adobe PDF(1200Kb) | 收藏 | 浏览/下载：526/94 | 提交时间：2018/12/25
Thermal-fluid-structure Coupling Thermal Elastoplastic Aerodynamic Pressure, Laser Damage Dynamic Rupture |
