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| 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
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高超声速进气道 不起动 再起动 主动射流 流动控制 |
| A new dynamic subgrid-scale model using artificial neural network for compressible flow 期刊论文
THEORETICAL AND APPLIED MECHANICS LETTERS, 2022, 卷号: 12, 期号: 4
Authors: Qi H(齐涵); Li XL(李新亮); Luo, Ning; Yu ZP(于长平)
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Subgrid-scale kinetic energy Eddy-viscosity model Compressible flow |
| Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(511Kb) | Favorite | View/Download：232/51 | Submit date：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors: Shi Weixiu; Pan LS(潘利生); Jin Suyi; Dong YH(董跃华); Li T(李腾); Zhao J(赵京); Wei XL(魏小林)
Adobe PDF(2198Kb) | Favorite | View/Download：288/65 | Submit date：2021/11/01
CO2-based mixture flammability laminar flame speed flammable critical mixing ratio transcritical power cycle |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮)
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Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| 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
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
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High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 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)
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Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
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hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Experimental Investigation on Flame Characterization and Temperature Profile of Single/Multiple Pool Fire in Cross Wind 期刊论文
JOURNAL OF THERMAL SCIENCE, 2020, 页码: 9
Authors: Chen Z(陈阵); Wei XL(魏小林); Li T(李腾)
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pool fire temperature profile flame characteristic kerosene cross wind |
| Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
Authors: Li GL(李广利); Cui K(崔凯); Xu YZ(徐应洲); Wang HX(王浩祥); Yang J(杨靖); Xu XG(许先贵)
Adobe PDF(661Kb) | Favorite | View/Download：412/101 | Submit date：2020/05/18 |
