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| 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 Authors: 王粤 ; 汪运鹏 ; 王春 ; 姜宗林![](/image/person.jpg)
Adobe PDF(4901Kb)  |   Favorite  |  View/Download:622/95  |  Submit date:2022/07/11 两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| 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)![](/image/person.jpg)
Adobe PDF(5479Kb)  |   Favorite  |  View/Download:446/86  |  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)![](/image/person.jpg)
Adobe PDF(9707Kb)  |   Favorite  |  View/Download:348/101  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 鼓包诱导斜爆震波的数值研究 期刊论文 推进技术, 2022, 卷号: 43, 期号: 05, 页码: 190-201 Authors: 韩信; 张文硕 ; 张子健; 刘云峰 ; 姜宗林![](/image/person.jpg)
Adobe PDF(3358Kb)  |   Favorite  |  View/Download:251/67  |  Submit date:2022/06/10 斜爆震发动机 鼓包 加速起爆 来流扰动 流动控制 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 Authors: Jiang ZL(姜宗林) ; Teng, Honghui
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| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 Authors: Lin MY(林明月); Wang C(王春) ; Peng J(彭俊); Jiang ZL(姜宗林)![](/image/person.jpg)
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| 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)![](/image/person.jpg)
Adobe PDF(3790Kb)  |   Favorite  |  View/Download:425/75  |  Submit date:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9 Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕) ; Han X(韩鑫); Liu YF(刘云峰) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(2608Kb)  |   Favorite  |  View/Download:281/122  |  Submit date:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良) ; Jiang ZL(姜宗林)![](/image/person.jpg)
View  |   Adobe PDF(4374Kb)  |   Favorite  |  View/Download:431/149  |  Submit date:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow 期刊论文 SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319 Authors: Xiang GX(项高翔); Wang C(王春) ; Teng HH(腾宏辉); Jiang ZL(姜宗林)![](/image/person.jpg)
View  |   Adobe PDF(1333Kb)  |   Favorite  |  View/Download:584/159  |  Submit date:2018/10/30 Supersonic Flow 3d Shock/shock Interaction 3d Asymmetrical Wave Configurations Spatial Dimension Reduction |