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高马赫数燃烧强化的激波风洞试验研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
作者:  张旭;  张启帆;  岳连捷;  孟东东;  罗苇航;  于江鹏;  张晓源;  李进平;  陈宏;  李飞
Adobe PDF(3069Kb)  |  收藏  |  浏览/下载:243/43  |  提交时间:2022/08/11
高马赫数  超声速燃烧  燃烧强化  小支板  JF-24激波风洞  
气相爆轰驱动二级轻气炮内弹道数值模拟 期刊论文
力学学报, 2022, 卷号: 54, 期号: 03, 页码: 810-821
作者:  尚甲豪;  邢好运;  汪球;  李进平;  赵伟;  魏炳忱
Adobe PDF(3263Kb)  |  收藏  |  浏览/下载:269/57  |  提交时间:2022/06/10
爆轰驱动  轻气炮  数值模拟  发射性能  内弹道  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  收藏  |  浏览/下载:337/49  |  提交时间:2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
作者:  Yu JP(于江鹏);  Li JP(李进平);  Wang Q(汪球);  Zhang SZ(张仕忠);  Zhang XY(张晓源)
Adobe PDF(3271Kb)  |  收藏  |  浏览/下载:247/48  |  提交时间:2021/11/01
Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
作者:  Wang Q(汪球);  Li JP(李进平);  Luo K(罗凯);  Li JW(栗继伟);  Zhao W(赵伟)
Adobe PDF(1158Kb)  |  收藏  |  浏览/下载:256/57  |  提交时间:2021/05/17
Hypersonic  Aerodynamic heating  Detached bow shock  Shock tube  expansion tube  
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:323/103  |  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  
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:302/65  |  提交时间:2020/08/26
two-stage light gas gun  detonation  quasi-one-dimensional  piston  projectile  
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
作者:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  收藏  |  浏览/下载:261/82  |  提交时间:2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow