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Experimental Study on Supersonic Combustion Characteristics of Al/B-Kerosene Nanofuels 期刊论文
AIAA JOURNAL, 2024, 页码: 9./通讯作者：Zhong, Fengquan
作者:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Gao ZB(高占彪)
收藏  |  浏览/下载：104/0  |  提交时间：2024/05/21
Plasma Assisted Combustion  Petroleum  Nanomaterials  Supersonic Combustor  Flow Measurement  Optical Properties  Boundary Layers  Hydrocarbon Fuels  Band Pass Filter  Heat and Mass Transfer  
Effect of cone rotation on the nonlinear evolution of Mack modes in supersonic boundary layers 期刊论文
JOURNAL OF FLUID MECHANICS, 2023, 卷号: 971, 页码: 48./通讯作者：Dong, Ming, Zhao, Lei
作者:  Song RJ(宋润杰);  Dong M(董明);  Zhao, Lei
Adobe PDF(3400Kb)  |  收藏  |  浏览/下载：255/33  |  提交时间：2023/10/16
boundary layer stability  supersonic flow  transition to turbulence  
Parametric study on wing-lambda-shock formation 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者:  Chainok S;  Rungroch T;  Chairach P;  Prapamonthon P;  Yooyen S;  Yin B(银波);  Yang GW(杨国伟);  Ju SJ(鞠胜军)
Adobe PDF(3026Kb)  |  收藏  |  浏览/下载：385/127  |  提交时间：2021/11/30
Shock  Supersonic flow  Transonic flow  
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10./通讯作者：Sun, Zhenxu
作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3818Kb)  |  收藏  |  浏览/下载：523/143  |  提交时间：2020/11/30
Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310./通讯作者：Sun, Zhenxu
作者:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  收藏  |  浏览/下载：443/125  |  提交时间：2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711./通讯作者：Li, XL
作者:  Chen XP;  Li XL(李新亮);  Zhu ZC
浏览  |  Adobe PDF(1844Kb)  |  收藏  |  浏览/下载：368/123  |  提交时间：2019/04/11
direct numerical simulation  velocity-temperature correlation  supersonic flow  channel flow  thermally perfect gas  strong Reynolds analogy  
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow 期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1333Kb)  |  收藏  |  浏览/下载：681/218  |  提交时间：2018/10/30
Supersonic Flow  3d Shock/shock Interaction  3d Asymmetrical Wave Configurations  Spatial Dimension Reduction  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun([email protected])
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：570/276  |  提交时间：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng([email protected])
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：379/117  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：351/108  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion