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| Turbulent burning velocity of NH3/H2/air mixtures spherical flames: Effects of differential diffusion and turbulent stretch 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 卷号: 59, 页码: 525-534 Authors: Cao, JianBin; Zhao, Nan Nan; Li, GuoXiu; Li, HongMeng; Zhang GP(张国鹏); Yang, Jun Favorite  |  View/Download:17/0  |  Submit date:2024/04/29 Ammonia/hydrogen/air mixtures Turbulent expending flame Differential diffusion Turbulent stretch Turbulent burning velocity |
| Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文 PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20 Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Wu WN(邬婉楠); Zhang QF(张启帆); Chen H(陈昊) Favorite  |  View/Download:49/0  |  Submit date:2024/03/11 |
| Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 139, 页码: 108383 Authors: Wang JL(王嘉麟); Han GL(韩桂来) Adobe PDF(5629Kb)  |  Favorite  |  View/Download:56/1  |  Submit date:2023/07/17 Hypersonic flow Tandem -arranged jets Streamline pattern Vortex structure Fuel -air mixing |
| Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations 期刊论文 INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2023, 卷号: 140, 页码: 14 Authors: Gao EK(高尔康); Fan WH(范文慧); Li X(李冼); Zhong FQ(仲峰泉) Adobe PDF(6628Kb)  |  Favorite  |  View/Download:180/6  |  Submit date:2023/02/09 Aviation kerosene Surface corrugation Convective heat transfer Supercritical conditions |
| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 Authors: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  Favorite  |  View/Download:413/78  |  Submit date:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |
| 基于主动射流控制的高超声速进气道再起动性能研究(英文) 期刊论文 Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662 Authors: 靳一超; 姚卫 Adobe PDF(1844Kb)  |  Favorite  |  View/Download:173/41  |  Submit date:2023/02/09 高超声速进气道 不起动 再起动 主动射流 流动控制 |
| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文 AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2434Kb)  |  Favorite  |  View/Download:330/88  |  Submit date:2022/08/23 Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 Authors: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY; Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:132/34  |  Submit date:2022/10/23 Hybrid rocket engine Swirl injection 11el composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 Authors: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY(张春元); Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:105/12  |  Submit date:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 氨燃料吸气式变循环发动机性能分析 期刊论文 力学学报, 2022, 卷号: 54, 页码: 16 Authors: 张鑫; 陆阳; 程迪; 范学军 Adobe PDF(1309Kb)  |  Favorite  |  View/Download:253/46  |  Submit date:2022/10/17 氨 涡轮模态 预冷模态 冲压模态 当量总热沉 当量热值 |