中文版 | English

在结果中检索

IMECH-IR
（本次检索基于用户作品认领结果）

浏览/检索结果: 共5条，第1-5条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8
作者:  Wang WT(王文韬);  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Gao, Liangjie;  Liu, Zhongchen;  Qian, Zhansen
收藏  |  浏览/下载：45/0  |  提交时间：2024/02/26
Finite Element Method  Hypersonic  Shock Tube/Tunnel  Diaphragm  Burst Pressure  
Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
作者:  Wang Q(汪球);  Olivier H;  Einhoff J;  Li JP(李进平);  Zhao W(赵伟)
浏览  |  Adobe PDF(1085Kb)  |  收藏  |  浏览/下载：415/100  |  提交时间：2019/05/29
Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic  
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
作者:  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1208Kb)  |  收藏  |  浏览/下载：620/130  |  提交时间：2018/10/30
copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic  
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
作者:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
浏览  |  Adobe PDF(468Kb)  |  收藏  |  浏览/下载：296/82  |  提交时间：2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(763Kb)  |  收藏  |  浏览/下载：531/227  |  提交时间：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone