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Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
作者:  Editors:Chen ZT;  Attri P;  Wang Q(汪球)
Adobe PDF(20682Kb)  |  收藏  |  浏览/下载:409/1  |  提交时间:2022/12/03
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载:105/2  |  提交时间:2023/03/23
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  收藏  |  浏览/下载:277/51  |  提交时间:2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
作者:  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
Adobe PDF(10792Kb)  |  收藏  |  浏览/下载:264/38  |  提交时间:2021/11/01
Shock wave  Turbulent boundary layer  Double compression ramp  Direct numerical simulation  
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV 期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
作者:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平);  Tong FL(童福林)
Adobe PDF(4454Kb)  |  收藏  |  浏览/下载:265/31  |  提交时间:2021/11/01
Lifting body model  Hypersonic transition  Direct numerical simulation  
Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 065111
作者:  段俊亦;  李欣;  李新亮;  刘洪伟
Adobe PDF(5069Kb)  |  收藏  |  浏览/下载:171/43  |  提交时间:2021/11/23
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:322/169  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner 期刊论文
JOURNAL OF TURBULENCE, 2020, 页码: 20
作者:  Tong FL(童福林);  Chen JQ;  Sun D;  Li XL(李新亮)
Adobe PDF(5228Kb)  |  收藏  |  浏览/下载:194/84  |  提交时间:2020/08/26
Wall-shear stress  expansion corner  supersonic turbulent boundary layer  direct numerical simulation  
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
作者:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
浏览  |  Adobe PDF(7909Kb)  |  收藏  |  浏览/下载:352/111  |  提交时间:2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner  
External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
作者:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
浏览  |  Adobe PDF(4679Kb)  |  收藏  |  浏览/下载:268/97  |  提交时间:2019/09/09