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A vibration isolator with a controllable quasi-zero stiffness region based on nonlinear force design 期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2024, 卷号: 45, 期号: 8, 页码: 1279-1294./通讯作者：Deng, Huaxia
Authors:  Lian, Xinyu;  Liu, Bing;  Deng HX(邓华夏);  Gong, Xinglong
Favorite  |  View/Download：15/0  |  Submit date：2024/08/23
low frequency  nonlinear  vibration isolator  quasi-zero stiffness (QZS)  O328  
Nanosphere Chain Model of Magnetic Fluid and Its Dynamic Performance 期刊论文
LANGMUIR, 2024, 卷号: 40, 期号: 12, 页码: 6187-6197./通讯作者：Deng, Huaxia, Gong, Xinglong
Authors:  Wang, Kang;  Liu, Bing;  Lian, Xinyu;  Xuan, Shouhu;  Deng, Huaxia;  Gong, Xinglong
Favorite  |  View/Download：103/0  |  Submit date：2024/04/29
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./通讯作者：Yue, Lianjie
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22./通讯作者：Zhang, Qifan
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
Authors:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
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高速进气道  低马赫数不起动  非定常  气动力  自起动  
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./通讯作者：Yue, Lianjie
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)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：283/75  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13./通讯作者：Yue, Lianjie
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
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Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:  Yang L;  岳连捷;  张启帆;  张新宇
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斜爆轰波的波角和法向速度-曲率关系初步探究 期刊论文
航空学报, 2020, 卷号: 41, 页码: 123701
Authors:  杨理;  岳连捷;  张新宇
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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10./通讯作者：Yue, Lianjie
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：418/138  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation