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背负式两体分离流动机理与安全分离方案研究 学位论文
博士论文,北京: 中国科学院大学, 2024
Authors:  王粤
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两级入轨  级间分离  高超声速  非定常流动  气动干扰  
Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Han GL(韩桂来)
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Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
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)
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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)
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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)  |  Favorite  |  View/Download:76/12  |  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
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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:419/44  |  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  
Dynamic shock interaction mechanism of stage separation for a two-stage-to-orbit vehicle in hypersonic flow 会议论文
空天飞行高温气动全国重点实验室(筹)2023年度夏季学术交流会暨高温气动学术前沿专题研讨会, 怀来, 2023-8-27 ~ 2023-8-29
Authors:  Wang Y(王粤);  Wang YP(汪运鹏)
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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)  |  Favorite  |  View/Download:67/11  |  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
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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