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| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷) ; Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇)
 Adobe PDF(3937Kb) |  Favorite | View/Download：233/62 | Submit date：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | Favorite | View/Download：287/86 | Submit date：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Design of a new supersonic biplane 期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
Authors: Zhai J; Zhang CA(张陈安); Wang FM(王发民); Zhang WW
Adobe PDF(5403Kb) | Favorite | View/Download：491/76 | Submit date：2020/06/08 |
| Separate and Combined Effects of Surface Roughness and Thermal Barrier Coating on Vane Cooling Performance 期刊论文
JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2020, 卷号: 12, 期号: 5, 页码: 15
Authors: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH
Adobe PDF(2963Kb) | Favorite | View/Download：347/124 | Submit date：2020/11/30
gas-turbine heat transfer surface roughness cooling performance thermal barrier coating |
| A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
Authors: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)
Adobe PDF(8566Kb) | Favorite | View/Download：229/62 | Submit date：2020/11/30
calorimeter shock tunnel heat transfer measurement hypersonic |
| Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors: Xue R; Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
Adobe PDF(3912Kb) | Favorite | View/Download：363/242 | Submit date：2020/08/26
Compressible boundary layer combustion Skin-friction reduction Boundary layer transition Transition k-kl-w model Hydrogen combustion |
| 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
Authors: Tong FL(童福林); Chen JQ; Sun D; Li XL(李新亮)
Adobe PDF(5228Kb) | Favorite | View/Download：215/93 | Submit date：2020/08/26
Wall-shear stress expansion corner supersonic turbulent boundary layer direct numerical simulation |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors: Yang L; 岳连捷; 张启帆; 张新宇
Adobe PDF(1289Kb) | Favorite | View/Download：240/64 | Submit date：2021/01/12 |
| Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors: Xue R(薛瑞); Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
Adobe PDF(3251Kb) | Favorite | View/Download：381/115 | Submit date：2020/07/06
Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction |
| Influence of domain size on direct numerical simulation of turbulent flow in a moderately curved concentric annular pipe 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 6, 页码: 21
Authors: Bagheri E; Wang BC; Yang ZX(杨子轩)
Adobe PDF(6795Kb) | Favorite | View/Download：213/105 | Submit date：2020/08/26 |
