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TSTO马赫7安全级间分离问题的数值研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542
Authors:  王粤;  汪运鹏;  薛晓鹏;  姜宗林
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两级入轨  高超声速  分离流动  气动干扰  级间分离  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
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Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
超常环境力学领域研究新进展—–《力学学报》极端力学专题研讨会综述报告 期刊论文
力学学报, 2021, 卷号: 53, 期号: 02, 页码: 589-599
Authors:  姜宗林;  刘俊丽;  苑朝凯;  陈海璇;  陆夕云
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极端力学  力学学报  超常环境力学领域  研究进展  研究展望  
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)
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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
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
基于深度学习技术的激波风洞智能测力系统研究 期刊论文
力学学报, 2020, 卷号: 52, 期号: 05, 页码: 1304-1313
Authors:  汪运鹏;  杨瑞鑫;  聂少军;  姜宗林
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激波风洞  人工智能  测力系统  动态校准  气动力测量  应变天平  
高超声速溢流冷却实验研究 期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
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高超声速热防护  主动冷却  溢流冷却  液膜  
Aerodynamic measurement of a large aircraft model in hypersonic flow 期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
长试验时间激波风洞测力技术研究 期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 545-556
Authors:  汪运鹏;  刘云峰;  苑朝凯;  罗长童;  王春;  胡宗民;  韩桂来;  赵伟;  姜宗林
View  |  Adobe PDF(8800Kb)  |  Favorite  |  View/Download:491/82  |  Submit date:2016/12/16
Shock Tunnel  Long-test Duration  Force Measurement  Strain-gaged Balance