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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
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：166/41  |  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  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  Favorite  |  View/Download：232/35  |  Submit date：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  Favorite  |  View/Download：402/65  |  Submit date：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
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：341/173  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:  Yao W(姚卫)
Adobe PDF(9586Kb)  |  Favorite  |  View/Download：657/295  |  Submit date：2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
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
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
Adobe PDF(4075Kb)  |  Favorite  |  View/Download：308/90  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
An efficient unstructured WENO method for supersonic reactive flows 期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
Adobe PDF(3673Kb)  |  Favorite  |  View/Download：415/98  |  Submit date：2018/10/30
Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction  
Theoretical analysis on deflagration-to-detonation transition 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 8, 页码: 84703
Authors:  Liu YF(刘云峰);  Shen H(沈还);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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deflagration  detonation  deflagration-to-detonation transition  
Influences of affiliated components and train length on the train wind 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
Authors:  Guo DL(郭迪龙);  Shang KM;  Zhang Y;  Yang GW(杨国伟);  Sun ZX(孙振旭);  Guo, DL
Adobe PDF(10201Kb)  |  Favorite  |  View/Download：297/121  |  Submit date：2017/09/04
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:  Liang JH(梁金虎);  Wang S(王苏);  Zhang ST(张胜涛);  Yue LJ(岳连捷);  Fan BC(范秉诚);  Zhang XY(张新宇);  Cui JP(崔季平);  Wang S(王苏)
Adobe PDF(1351Kb)  |  Favorite  |  View/Download：889/218  |  Submit date：2014/08/14
Ignition Delay  Vitiation Effect  Kerosene  Water  Carbon Dioxide  Shock Tube