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| Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
作者: 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) |  收藏 | 浏览/下载：263/60 | 提交时间：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
作者: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮)
Adobe PDF(4402Kb) | 收藏 | 浏览/下载：206/48 | 提交时间：2021/06/07
Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林)
Adobe PDF(3790Kb) | 收藏 | 浏览/下载：397/63 | 提交时间：2021/03/03
Hypersonics Shock tunnels Flow characteristics |
| 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
作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | 收藏 | 浏览/下载：335/172 | 提交时间：2021/03/30
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
作者: 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) | 收藏 | 浏览/下载：204/51 | 提交时间：2021/03/30
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
作者: 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)
Adobe PDF(1090Kb) | 收藏 | 浏览/下载：261/101 | 提交时间：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Study of coupled effect of impingement jet cooling of kerosene with solid structure 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
作者: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇)
 浏览 | Adobe PDF(2806Kb) | 收藏 | 浏览/下载：371/92 | 提交时间：2020/03/21
impingement jet cooling hydrocarbon fuel heat transfer enhancement fluid-solid coupling |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
浏览 | Adobe PDF(4075Kb) | 收藏 | 浏览/下载：305/89 | 提交时间：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
作者: Chen XP; Li XL(李新亮); Zhu ZC
浏览 | Adobe PDF(1844Kb) | 收藏 | 浏览/下载：318/101 | 提交时间：2019/04/11
direct numerical simulation velocity-temperature correlation supersonic flow channel flow thermally perfect gas strong Reynolds analogy |
| Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
作者: Yuan CK(苑朝凯); Zhou K(周凯); Liu YF(刘云峰); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(1468Kb) | 收藏 | 浏览/下载：344/101 | 提交时间：2019/04/11
Spectral measurement Hypervelocity flow Radiation Expansion tunnel |
