IMECH-IR

浏览/检索结果: 共3条,第1-3条 帮助

限定条件                    
已选(0)清除 条数/页:   排序方式:
Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
作者:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
Adobe PDF(4178Kb)  |  收藏  |  浏览/下载:288/67  |  提交时间:2021/11/15
Strain  Balance  Milli-newton  Design  Calibration  
页岩气开采中的若干力学前沿问题 期刊论文
力学进展, 2019, 卷号: 49, 期号: 00, 页码: 1-236
作者:  刘曰武;  高大鹏;  李奇;  万义钊;  段文杰;  曾霞光;  李明耀;  苏业旺;  范永波;  李世海;  鲁晓兵;  周东;  陈伟民;  傅一钦;  姜春晖;  侯绍继;  潘利生;  魏小林;  胡志明;  端祥刚;  高树生;  沈瑞;  常进;  李晓雁;  柳占立;  魏宇杰;  郑哲敏
Adobe PDF(109408Kb)  |  收藏  |  浏览/下载:302/39  |  提交时间:2019/09/12
页岩气  压裂  力学性质  数值模拟  监测技术  渗流  
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
作者:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
浏览  |  Adobe PDF(1159Kb)  |  收藏  |  浏览/下载:200/66  |  提交时间:2017/05/27
All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing