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| Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation 期刊论文
Acta Astronautica, 2024, 卷号: 216, 页码: 488-503
Authors: Wang Y(王粤) ; Wang YP(汪运鹏)
 Adobe PDF(18431Kb) |  Favorite | View/Download：107/19 | Submit date：2024/01/18
Multibody separation Hypersonic Dynamic stability Center of pressure Aerodynamic interaction Numerical simulation |
| 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)
Adobe PDF(7258Kb) | Favorite | View/Download：91/18 | Submit date：2024/01/15
Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| Computational study of lateral jet interaction in hypersonic thermochemical non-equilibrium flows using nonlinear coupled constitutive relations 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 14
Authors: Zeng, Shuhua; Yang, Junyuan; Zhao, Wenwen; Huang YF(黄依峰); Jiang, Zhongzheng; Chen, Weifang
Adobe PDF(3990Kb) | Favorite | View/Download：81/9 | Submit date：2024/01/22 |
| DeepStSNet: Reconstructing the quantum state-resolved thermochemical nonequilibrium flowfield using deep neural operator learning with scarce data 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2023, 卷号: 491, 页码: 112344
Authors: Lv JQ(吕家琦); Hong QZ(洪启臻); Wang XY(王小永); Mao, Zhiping; Sun QH(孙泉华)
Adobe PDF(5558Kb) | Favorite | View/Download：74/2 | Submit date：2023/09/26
Hypersonic Thermochemical nonequilibrium State-to-state approach Deep learning Multiphysics Data assimilation |
| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
Authors: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民); Han GL(韩桂来)
Adobe PDF(8946Kb) | Favorite | View/Download：84/5 | Submit date：2023/11/28
oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors: 王粤; 汪运鹏; 姜宗林
Adobe PDF(6797Kb) | Favorite | View/Download：380/39 | Submit date：2022/12/01
两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| 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 |
| 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 |
| 变工况下超燃冲压发动机突变及迟滞特性研究 学位论文
博士论文，北京: 中国科学院大学, 2022
Authors: 吴振杰
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超燃冲压发动机 变工况 突变 迟滞 起动特性 |
| 高焓空气等离子体放电若干关键问题研究 学位论文
博士论文，北京: 中国科学院大学, 2022
Authors: 韩宁
Favorite | View/Download：173/6 | Submit date：2022/11/21
高焓空气等离子体 感应耦合等离子体发生器 稳定放电 稀薄流场密度估算 石墨保型烧蚀 |
