|
Selected(0)Clear
Items/Page: Sort: |
| Improving reservoir permeability by electric pulse controllable shock wave 期刊论文
JOURNAL OF PETROLEUM EXPLORATION AND PRODUCTION TECHNOLOGY, 2023, 页码: 01633
Authors: Zhu XG(朱心广); Feng C(冯春) ; Cheng PD(程鹏达)
 Adobe PDF(1468Kb) |  Favorite | View/Download：68/4 | Submit date：2023/06/15
Controllable shock wave continuous-discontinuous element method Coupling model Fracture Reservoir permeability |
| 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：358/104 | Submit date：2022/11/14
Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 可重构力学超材料的设计与波动特性研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 10, 页码: 2708-2716
Authors: 肖伯雅; 杨洮; 冯亚菲; 刘宇; 徐文帅; 陈猛; 姜恒; 王育人
Adobe PDF(1304Kb) | Favorite | View/Download：402/70 | Submit date：2022/11/14
力学超材料 双稳态 色散 带隙 主动调控 |
| A hybrid kinetic WGVC-WENO scheme for compressible flows 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 12
Authors: He K(何康); Liu HW(刘洪伟); Li XL(李新亮)
Adobe PDF(2656Kb) | Favorite | View/Download：336/66 | Submit date：2021/11/01
Gas kinetic theory WGVC-WENO methods Hybrid flux Numerical dissipation |
| Impact resistance of single-layer metallic glass nanofilms to high-velocity micro-particle penetration 期刊论文
EXTREME MECHANICS LETTERS, 2021, 卷号: 44, 页码: 6
Authors: Dong JL(董金磊); Song X(宋鑫); Wang, Z. J.; Xiao KL(肖凯璐); Liu, Y. H.; Wilde, G.; Wu XQ(吴先前); 蒋敏强2,4)
 Adobe PDF(2174Kb) | Favorite | View/Download：431/74 | Submit date：2021/05/31
Metallic glass nanofilm High-velocity impact Penetration Impact resistance |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童)
Adobe PDF(1806Kb) | Favorite | View/Download：311/70 | Submit date：2021/05/17
Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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 |
| Parametric study on wing-lambda-shock formation 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
Authors: Chainok S; Rungroch T; Chairach P; Prapamonthon P; Yooyen S; Yin B(银波); Yang GW(杨国伟); Ju SJ(鞠胜军)
Adobe PDF(3026Kb) | Favorite | View/Download：313/102 | Submit date：2021/11/30
Shock Supersonic flow Transonic flow |
| 高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors: 汪运鹏; 姜宗林
Adobe PDF(2086Kb) | Favorite | View/Download：260/76 | Submit date：2021/01/29 |
| 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：296/135 | Submit date：2020/09/27
Dynamic zone flamelet model Supersonic hydrogen jet Large eddy simulation Supersonic combustion Turbulent combustion model |
