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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)
Favorite  |  View/Download:0/0  |  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)
Favorite  |  View/Download:18/0  |  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)
Favorite  |  View/Download:18/0  |  Submit date:2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing 期刊论文
POLYMER TESTING, 2019, 卷号: 77, 页码: 8
Authors:  Yang D;  Ren JK;  Li JW(栗继伟);  Wang QL;  Wang Q(汪球);  Xie Z;  Qu XZ
View  |  Adobe PDF(2608Kb)  |  Favorite  |  View/Download:59/4  |  Submit date:2019/11/25
Pressure sensitive paint (PSP)  Bi-layer structured coating  Fast-response  Self-referenced measurement  
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1208Kb)  |  Favorite  |  View/Download:231/37  |  Submit date:2018/10/30
copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic  
高超声速绕平板直立舵干扰气动热研究 期刊论文
中北大学学报(自然科学版), 2017, 卷号: 38, 期号: 05, 页码: 609-613
Authors:  栗继伟;  汪球;  赵伟
View  |  Adobe PDF(1022Kb)  |  Favorite  |  View/Download:140/24  |  Submit date:2017/12/22
高超声速  激波/边界层干扰  气动热  激波风洞  
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:199/31  |  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:125/27  |  Submit date:2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics