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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:365/179  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Specific signal imaging velocimetry for rarefied plasma flows 期刊论文
EXPERIMENTS IN FLUIDS, 2020, 卷号: 61, 期号: 12, 页码: 247
作者:  Cao JW(曹进文);  Huang HJ(黄河激);  Pan WX(潘文霞);  Meng X(孟显);  Wu CK(吴承康)
Adobe PDF(4736Kb)  |  收藏  |  浏览/下载:308/93  |  提交时间:2020/12/28
MOLECULAR TAGGING VELOCIMETRY  MACH PROBE  VELOCITY  TURBULENT  JETS  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:290/102  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
An improved weighted essentially non-oscillatory scheme with modified smoothness indicator tau and adaptive index p 期刊论文
INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 2020, 页码: 15
作者:  Li X(李欣);  Yu ZP(于长平);  Li L;  Li XL(李新亮)
Adobe PDF(3965Kb)  |  收藏  |  浏览/下载:317/107  |  提交时间:2020/06/15
WENO scheme  high resolution  shock-capturing  smoothness indicator  adaptive optimisation