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| 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 |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | 收藏 | 浏览/下载：239/67 | 提交时间：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945
作者: Xiang GX(项高翔); Yang PF(杨鹏飞); Teng HH(滕宏辉); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(1871Kb) | 收藏 | 浏览/下载：512/148 | 提交时间：2019/09/09
Al particle cellular detonation heat capacity hybrid model |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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
作者: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH
Adobe PDF(2963Kb) | 收藏 | 浏览/下载：300/104 | 提交时间：2020/11/30
gas-turbine heat transfer surface roughness cooling performance thermal barrier coating |
| Flame Extinction of Spherical PMMA in Microgravity: Effect of Fuel Diameter and Conduction 期刊论文
MICROGRAVITY SCIENCE AND TECHNOLOGY, 2020, 页码: 11
作者: Wu CJ(吴传嘉); Sun PY; Wang XZ(王秀珍); Huang XY; Wang SF(王双峰)
Adobe PDF(1591Kb) | 收藏 | 浏览/下载：269/97 | 提交时间：2020/11/30
Spacecraft fire Plastic fuel Drop tower Curvature effect Heat conduction |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | 收藏 | 浏览/下载：312/100 | 提交时间：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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
作者: 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) | 收藏 | 浏览/下载：178/42 | 提交时间：2020/11/30
calorimeter shock tunnel heat transfer measurement hypersonic |
| Three-dimensional simulation of ligament formation and breakup caused by external vibration 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 8, 页码: 17
作者: Li YK; Zhang M; Wu K(吴坤)
Adobe PDF(14652Kb) | 收藏 | 浏览/下载：371/83 | 提交时间：2020/10/23 |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
作者: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(7457Kb) | 收藏 | 浏览/下载：242/87 | 提交时间：2020/07/06
Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
