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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:218/56  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文 AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430 Authors: Jiang YZ; Wen CY; Zhang DL(张德良) Adobe PDF(6207Kb)  |  Favorite  |  View/Download:264/102  |  Submit date:2021/02/09 |
| Unsteady combustion mode with a super-high frequency induced by a curved shock 期刊论文 PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 116101 Authors: Teng HH(滕宏辉); Liu S; Zhang ZJ(张子健) Adobe PDF(5194Kb)  |  Favorite  |  View/Download:270/72  |  Submit date:2020/12/28 PROJECTILE MECHANISM SYSTEMS |
| 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:275/117  |  Submit date:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Development and application of ANN model for property prediction of supercritical kerosene 期刊论文 Computers and Fluids, 2020, 卷号: 209, 期号: 2020, 页码: 1-18 Authors: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(10546Kb)  |  Favorite  |  View/Download:357/126  |  Submit date:2020/08/27 Artificial Neural Network (Ann) Principle Of Extended Corresponding State (Ecs) Rp-3 Kerosene Superitical Pressure Openfoam |
| 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:343/107  |  Submit date: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 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:209/51  |  Submit date:2020/11/30 calorimeter shock tunnel heat transfer measurement hypersonic |
| On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955 Authors: Yao W(姚卫) Adobe PDF(3791Kb)  |  Favorite  |  View/Download:284/133  |  Submit date:2020/09/27 Dynamic zone flamelet model Supersonic hydrogen jet Large eddy simulation Supersonic combustion Turbulent combustion model |
| A multi-time scale solution strategy for an elastomeric aircraft 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13 Authors: Yang L(杨磊); Sun QH(孙泉华) Adobe PDF(1858Kb)  |  Favorite  |  View/Download:225/90  |  Submit date:2020/08/26 Flight dynamic simulation Multi-time scale Elastomeric aircraft Reduced order models Store separation |
| Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文 INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8 Authors: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇) Adobe PDF(2316Kb)  |  Favorite  |  View/Download:287/115  |  Submit date:2020/08/26 Impingement jets Kerosene Heat transfer coefficient Pressure loss Reynolds number |