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Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
Authors:  Guo SQ(郭帅旗);  Liu W(刘文);  Zhang CA(张陈安);  Liu Y(刘洋);  Wang FM(王发民)
Favorite  |  View/Download：34/0  |  Submit date：2024/02/05
Hypersonic waverider  Aerodynamic model  Symbolic regression  Bluntness effect  
Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades 期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680
Authors:  Qu DD(屈丹丹);  Lin X(林鑫);  Zhang K(张坤);  Li ZY(李志永);  Wang ZZ(王泽众);  Liu GL(刘国亮);  Meng Y(孟洋);  Luo GX(罗耕星);  Wang RY(王若岩);  Yu XL(余西龙)
Adobe PDF(4980Kb)  |  Favorite  |  View/Download：178/5  |  Submit date：2023/09/05
Hybrid rocket engine  additive manufacturing  three-dimensional printing  breathable blade  composite fuel grain  mechanical and combustion properties  porous structure  >  
Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124
Authors:  Wang DG(王大高);  Han GL(韩桂来);  Liu MK(刘美宽);  Jiang ZL(姜宗林)
Adobe PDF(10056Kb)  |  Favorite  |  View/Download：65/4  |  Submit date：2023/09/26
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:  Yuan CK(苑朝凯);  Meng FZ(孟凡钊);  Liu, Xu;  Liu YF(刘云峰);  Lian H(连欢);  Liu, Yingzheng;  Peng, Di
Adobe PDF(3477Kb)  |  Favorite  |  View/Download：62/7  |  Submit date：2023/07/17
Temperature-sensitive paint  Heat flux  Conjugate gradient method  Air-breathing hypersonic vehicle  Inverse heat conduction problem  
Conversion of carbon dioxide in atmospheric pressure dielectric barrier discharges with different electrode configurations 期刊论文
PHYSICA SCRIPTA, 2023, 卷号: 98, 期号: 8, 页码: 85605
Authors:  Wang C(王超);  Wang, HaiXing;  Liu CY(刘昌裕);  Meng X(孟显);  Jin, GuangYuan;  Huang HJ(黄河激);  Cao JW(曹进文);  Sun, SuRong;  Yan C(闫聪)
Adobe PDF(1955Kb)  |  Favorite  |  View/Download：49/5  |  Submit date：2023/09/05
carbon dioxide decomposition  DBD  electrode configuration  
Density estimation of an ultrahigh-speed rarefied flow field based on force analysis of a pendulum sphere 期刊论文
VACUUM, 2023, 卷号: 211, 页码: 111919
Authors:  Han N(韩宁);  Cao JW(曹进文);  Meng X(孟显);  Liu HL(刘宏立);  Zhang SH(张少华);  Huang HJ(黄河激)
Adobe PDF(3867Kb)  |  Favorite  |  View/Download：51/9  |  Submit date：2023/06/15
Density estimation  Pendulum sphere  Force analysis  Ultrahigh-speed rarefied flow  
Experimental study of the effect of dielectric materials on the decomposition of carbon dioxide in a dielectric barrier discharge 期刊论文
PLASMA SOURCES SCIENCE & TECHNOLOGY, 2023, 卷号: 32, 期号: 2, 页码: 25011
Authors:  Liu, ChangYu;  Wang, HaiXing;  Wang, Chao;  Meng X(孟显);  Huang HJ(黄河激);  Cao JW(曹进文);  Sun, SuRong;  Yan C(闫聪)
Adobe PDF(5921Kb)  |  Favorite  |  View/Download：53/5  |  Submit date：2023/04/20
carbon dioxide decomposition  DBD  relative permittivity  
Numerical investigation on unsteady interaction of oblique/bow shock during rotation based on non-inertial coordinate system 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 9
Authors:  Wang DG(王大高);  Han GL(韩桂来);  Liu MK(刘美宽);  Jiang ZL(姜宗林)
Adobe PDF(3151Kb)  |  Favorite  |  View/Download：223/48  |  Submit date：2023/02/03
Experimental study of the spray characteristics of twin-fluid atomization: Focusing on the annular flow regime 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 21
Authors:  Liu C(刘畅);  Wu K(吴坤);  Zhang, Zhenyu;  Yuan YM(袁越明);  Fan XJ(范学军)
Adobe PDF(14059Kb)  |  Favorite  |  View/Download：184/33  |  Submit date：2023/02/27
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
Authors:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  Favorite  |  View/Download：123/27  |  Submit date：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance