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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
Authors:  尚甲豪;  邢好运;  汪球;  李进平;  赵伟;  魏炳忱
Adobe PDF(3263Kb)  |  Favorite  |  View/Download：312/67  |  Submit date：2022/06/10
爆轰驱动  轻气炮  数值模拟  发射性能  内弹道  
Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:  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)  |  Favorite  |  View/Download：280/63  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：343/107  |  Submit date：2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
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
Authors:  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)  |  Favorite  |  View/Download：308/67  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：274/85  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download：412/77  |  Submit date：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
View  |  Adobe PDF(468Kb)  |  Favorite  |  View/Download：317/86  |  Submit date：2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
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：464/78  |  Submit date：2016/12/16
Shock Tunnel  Long-test Duration  Force Measurement  Strain-gaged Balance  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(532Kb)  |  Favorite  |  View/Download：654/159  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
高焓激波风洞喷管流场非平衡特性研究 期刊论文
空气动力学学报, 2015, 卷号: 33, 期号: 1, 页码: 66-71
Authors:  汪球;  赵伟;  滕宏辉;  姜宗林
View  |  Adobe PDF(1866Kb)  |  Favorite  |  View/Download：510/110  |  Submit date：2015/11/02
爆轰驱动  非平衡  焓值  激波风洞