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:
A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020
作者:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:145/39  |  提交时间:2021/02/01
JF12复现风洞平板边界层转捩研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
作者:  刘美宽;  韩桂来;  姜宗林
浏览  |  Adobe PDF(1326Kb)  |  收藏  |  浏览/下载:467/89  |  提交时间:2019/11/21
激波风洞  边界层  转捩  
Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang Q(汪球);  Lu P(卢盼);  Li JW(栗继伟);  Wu S(吴松);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
Adobe PDF(299Kb)  |  收藏  |  浏览/下载:83/33  |  提交时间:2023/03/17
One-Step Direct Aeroacoustic Simulation Using Space-Time Conservation Element and Solution Element Method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Ho CY;  Leung RCK;  Zhou K;  Lam GCY;  Jiang ZL(姜宗林)
Adobe PDF(400Kb)  |  收藏  |  浏览/下载:494/200  |  提交时间:2014/01/14
Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
Computational flow visualization of shock wave motions 会议论文
24th International Congress on High-Speed Photography and Photonics, SENDAI, JAPAN, SEP 24-29, 2000
作者:  Jiang ZL(姜宗林);  Takayama K;  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(745Kb)  |  收藏  |  浏览/下载:148/56  |  提交时间:2016/06/30