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| 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
作者: Song RJ(宋润杰); Dong M(董明); Zhao, Lei
 Adobe PDF(3400Kb) |  收藏 | 浏览/下载：59/1 | 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：270/86 | 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
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：407/103 | 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
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：312/83 | 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
作者: Chen XP; Li XL(李新亮); Zhu ZC
 浏览 | Adobe PDF(1844Kb) | 收藏 | 浏览/下载：308/95 | 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)
 Adobe PDF(1333Kb) | 收藏 | 浏览/下载：517/128 | 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(xfan@imech.ac.cn)
Adobe PDF(1173Kb) | 收藏 | 浏览/下载：434/214 | 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(pengzhang.zhang@polyu.edu.hk)
浏览 | Adobe PDF(1249Kb) | 收藏 | 浏览/下载：294/87 | 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：268/80 | 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 |
| Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
浏览 | Adobe PDF(468Kb) | 收藏 | 浏览/下载：292/81 | 提交时间：2018/01/16
Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
