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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
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:334/172  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  收藏  |  浏览/下载:250/74  |  提交时间:2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
Thermodynamic optimization of Rankine cycle using CO2-based binary zeotropic mixture for ocean thermal energy conversion 期刊论文
APPLIED THERMAL ENGINEERING, 2020, 卷号: 178, 页码: 15
作者:  Li CY;  Pan LS(潘利生);  Wang YZ
Adobe PDF(2059Kb)  |  收藏  |  浏览/下载:286/130  |  提交时间:2020/08/26
OTEC (Ocean Thermal Energy Conversion)  CO2-based mixture  Performance evaluation  Optimization design  
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者:  Luo K(罗凯);  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2023Kb)  |  收藏  |  浏览/下载:321/102  |  提交时间:2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
作者:  Zhang SZ(张仕忠);  Wang Q(汪球);  Li JP(李进平);  Zhang XY(张晓源);  Chen H(陈宏)
Adobe PDF(8566Kb)  |  收藏  |  浏览/下载:189/45  |  提交时间:2020/11/30
calorimeter  shock tunnel  heat transfer measurement  hypersonic  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:260/101  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
作者:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  收藏  |  浏览/下载:348/112  |  提交时间:2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction  
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
作者:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(2084Kb)  |  收藏  |  浏览/下载:349/79  |  提交时间:2020/07/06
Large-eddy simulation  Subgrid-scale model  Rotating turbulent channel flow  
Performance and Modeling of a Two-Stage Light Gas Gun Driven by Gaseous Detonation 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 12, 页码: 16
作者:  Tang WQ(唐伟奇);  Wang Q(汪球);  Wei BC(魏炳忱);  Li JW(栗继伟);  Li JP(李进平);  Shang JH(尚甲豪);  Zhang K(张坤);  Zhao W(赵伟)
Adobe PDF(6798Kb)  |  收藏  |  浏览/下载:300/64  |  提交时间:2020/08/26
two-stage light gas gun  detonation  quasi-one-dimensional  piston  projectile  
矩形隔离段激波串非对称性及迟滞特性研究 学位论文
博士论文,北京: 中国科学院大学, 2020
作者:  黄庭隆
Adobe PDF(13697Kb)  |  收藏  |  浏览/下载:281/10  |  提交时间:2020/05/31
激波串  非对称  激波串迟滞  隔离段  斜楔