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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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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)
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View/Download:109/19
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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)
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View/Download:92/18
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Submit date:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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View/Download:46/6
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
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)
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View/Download:81/9
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Submit date:2024/01/22
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)
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View/Download:381/39
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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
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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View/Download:52/5
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
高压捕获翼翼面形状优化研究
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
张凯凯
Adobe PDF(4891Kb)
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Submit date:2023/06/29
高超声速滑翔飞行器,高压捕获翼,气动性能,单目标优化,多目标优化
高超声速气动弹性响应及热环境下的颤振特性研究
学位论文
博士论文,北京: 中国科学院大学, 2023
Authors:
黄杰
Adobe PDF(8448Kb)
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View/Download:108/2
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Submit date:2023/06/26
高超声速飞行器
气动-热-结构耦合
壁板颤振
TPS壁板
直接积分法
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)
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View/Download:209/67
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Submit date:2023/05/26
Two-stage-to-orbit
Hypersonic
Numerical simulation
Stage separation
Aerodynamic interaction
Unsteady flow
Center of gravity
高速飞行器结构噪声激励热态动力学行为研究
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
刘聪
Adobe PDF(6835Kb)
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View/Download:143/6
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Submit date:2023/06/13
高超声速飞行器,圆柱壳夹层板结构,热噪声环境,频域分析方法,结构动力学响应