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混合边界条件下的空泡及约束界面响应研究 学位论文
硕士论文,北京: 中国科学院大学, 2020
Authors:  李泓辰
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空泡动力学,气液界面,射流,界面不稳定性,流固耦合  
Dynamic behaviors of a laser-induced bubble and transition mechanism of collapse patterns in a tube 期刊论文
AIP ADVANCES, 2020, 卷号: 10, 期号: 3, 页码: 11
Authors:  Li HC(李泓辰);  Huang J(黄荐);  Wu XQ(吴先前);  Zhang J(张健);  Wang JZ(王静竹);  Wang YW(王一伟);  Huang CG(黄晨光)
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单空泡与自由液面相互作用规律研究进展 期刊论文
力学学报, 2019, 卷号: 51, 期号: 06, 页码: 1682-1698
Authors:  郭文璐;  李泓辰;  王静竹;  王一伟;  黄晨光
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非球形演化  自由面变形  细射流  粗射流  冠状水裙  
类球形空泡的动态特征识别与分析 会议论文
北京力学会第二十五届学术年会, 中国北京, 2019年1月6日
Authors:  李泓辰;  杨明;  刘鹏;  王静竹;  王一伟
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电火花空化  空泡动力学  圆形检测  软物质  
H-S管对超声速欠膨胀自由射流的激励 期刊论文
兰州理工大学学报, 2016, 卷号: 42, 期号: 03, 页码: 167-172
Authors:  顾声龙;  吴玉帅;  陈立红;  张新宇
View  |  Adobe PDF(2865Kb)  |  Favorite  |  View/Download:57/7  |  Submit date:2017/12/26
超声速射流  激励  纹影  H-s管  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
双模态发动机的模态鉴别方法 期刊论文
力学学报, 2015, 期号: 3, 页码: 389-397
Authors:  李飞;  王知溥;  余西龙;  顾洪斌;  陈立红;  张新宇
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双模态冲压发动机  模态鉴别  释热分布  
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
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Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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局部收缩比一致的变截面高超声速内转式进气道 专利
发明专利. 局部收缩比一致的变截面高超声速内转式进气道, 专利号: ZL201210157992.X, 申请日期: 2012-05-21, 授权日期: 2014-06-13
Inventors:  肖雅彬;  岳连捷;  卢洪波;  陈立红;  张新宇
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