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4条，第1-4条 帮助

限定条件                
已选(0)清除 条数/页：   排序方式：
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：336/173  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
作者:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(2166Kb)  |  收藏  |  浏览/下载：438/112  |  提交时间：2017/11/16
Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles 期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
作者:  Luo CT(罗长童);  Hu ZM(胡宗民);  Zhang SL;  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1001Kb)  |  收藏  |  浏览/下载：339/119  |  提交时间：2016/01/07
Aerodynamic Coefficient  Data Correlation  Scaling Parameter  Genetic Programming  Invariant  
Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability 期刊论文
Advances in Applied Mathematics and Mechanics, 2014, 卷号: 6, 期号: 6, 页码: 718-731
作者:  Dou HS;  Hu ZM(胡宗民);  Khoo BC;  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(487Kb)  |  收藏  |  浏览/下载：801/257  |  提交时间：2014/11/27
Numerical Simulation  Detonation  Ddt  Energy Release  Duct