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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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微重力重点实验室 [2]
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姚卫 [2]
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A measurement of Hubble constant using cosmographic approach combining fast radio bursts and supernovae
期刊论文
MONTHLY NOTICES OF THE ROYAL ASTRONOMICAL SOCIETY, 2024, 卷号: 527, 期号: 3, 页码: 7861-7870./通讯作者:Xu, Lixin
Authors:
Gao, Jiaze
;
Zhou, Zhihuan
;
Du MH(杜明辉)
;
Zou, Rui
;
Hu, Jianping
;
Xu, Lixin
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View/Download:131/0
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Submit date:2024/03/11
cosmology: cosmological parameters
transients: fast radio bursts
Mechanical strength determines Ca2+ transients triggered by the engagement of beta(2) integrins to their ligands
期刊论文
EXPERIMENTAL CELL RESEARCH, 2020, 卷号: 387, 期号: 2, 页码: 7./通讯作者:Long, Mian
Authors:
Shu XY(舒芯钰)
;
Li N(李宁)
;
Huang DD(黄丹丹)
;
Zhang Y(章燕)
;
Lv SQ(吕守芹)
;
Long M(龙勉)
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Adobe PDF(1108Kb)
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View/Download:567/210
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Submit date:2020/04/07
beta(2) integrin
Ligands
Calcium transients
Bond strength
Mechanotransduction
Shear stress
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(
[email protected]
)
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  |  
Adobe PDF(1173Kb)
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View/Download:538/250
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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View/Download:576/205
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Understanding the enhancement of coating's thermal cracking resistance by multiple segmentation
会议论文
2011 International Conference on Advanced Design and Manufacturing Engineering, ADME 2011, Guangzhou, China, SEP 16-18, 2011
Authors:
Chen XJ(陈学军)
;
Chen GN(陈光南)
;
Chen XJ(陈学军)
Adobe PDF(325Kb)
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View/Download:819/198
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Submit date:2013/02/26
Coatings
Crack Initiation
Cracking (Chemical)
Cracks
Design
Finite Element Method
Stress Intensity Factors
Thermal Shock
Thermal Stress
Cracking Behavior
Driving Forces
Experimental Observation
Hollow Cylinders
Multiple Segmentation
Outer Surface
Principle Of Superposition
Segmentation Crack
Segmentation Cracks
Segmented Coatings
Steady State
Thermal Cracking
Thermal Shock Resistance
Thermal Transients