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| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors: Yao W(姚卫) ; Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬)
 Adobe PDF(2954Kb) |  Favorite | View/Download：313/78 | Submit date：2021/11/15
Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
 Adobe PDF(8067Kb) | Favorite | View/Download：432/84 | Submit date：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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
Authors: 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) | Favorite | View/Download：283/123 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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
Authors: 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) | Favorite | View/Download：367/113 | Submit date：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1657Kb) | Favorite | View/Download：293/103 | Submit date：2020/08/26
Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
 View | Adobe PDF(2165Kb) | Favorite | View/Download：434/101 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
View | Adobe PDF(2110Kb) | Favorite | View/Download：403/143 | Submit date：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
View | Adobe PDF(1937Kb) | Favorite | View/Download：281/90 | Submit date：2018/10/30
Hypersonic Shock tunnel Start-up process Impulse force Vibration |
| The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors: Li HX(李慧鑫); Ye L(叶亮); Wei XL(魏小林); Li T(李腾); Li S(李森); Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View | Adobe PDF(1708Kb) | Favorite | View/Download：515/221 | Submit date：2017/12/18
H2o2/kerosene Bipropellant Coaxial-swirl Injector Geometric Constant Performance |
