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Wall shear stress and wall heat flux in a supersonic turbulent boundary layer subjected to concave surface curvature 期刊论文
PHYSICAL REVIEW FLUIDS, 2023, 卷号: 8, 期号: 12, 页码: 29
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Ji XX(纪相鑫);  Dong, Siwei;  Yuan, Xianxu;  Li XL(李新亮)
Adobe PDF(7538Kb)  |  Favorite  |  View/Download：59/6  |  Submit date：2024/01/22
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：49/6  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Two-stage-to-orbit  Hypersonic  Numerical simulation  Stage separation  Aerodynamic interaction  Unsteady flow  Center of gravity  
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：400/77  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：166/41  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  Favorite  |  View/Download：321/93  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：326/87  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
基于高温真实气体效应的双锥磁流体流动控制 期刊论文
航空学报, 2022, 卷号: 43, 期号: S2, 页码: 79-91
Authors:  罗凯;  汪球;  李进平;  赵伟
Adobe PDF(1945Kb)  |  Favorite  |  View/Download：137/48  |  Submit date：2023/02/09
磁流体  流动控制  双锥流动  高温真实气体效应  洛伦兹力  
基于高温真实气体效应双锥MHD流动控制研究 期刊论文
航空学报, 2022, 页码: 14
Authors:  罗凯;  汪球;  李进平;  赵伟
Adobe PDF(1326Kb)  |  Favorite  |  View/Download：199/49  |  Submit date：2022/10/17
磁流体  流动控制  双锥流动  高温真实气体效应  洛伦兹力  
Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(3187Kb)  |  Favorite  |  View/Download：253/84  |  Submit date：2021/10/29