2014
DOI: 10.1016/j.compositesb.2013.08.063
|View full text |Cite
|
Sign up to set email alerts
|

Hysteresis loop model of unidirectional carbon fiber-reinforced ceramic matrix composites under an arbitrary cyclic load

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
6
0

Year Published

2017
2017
2022
2022

Publication Types

Select...
8

Relationship

2
6

Authors

Journals

citations
Cited by 28 publications
(6 citation statements)
references
References 16 publications
0
6
0
Order By: Relevance
“…Based on the comprehensive analysis, it is found that there are two main energy-consuming methods for fluid damping: One is the gap flow, which achieves the energy consumption by the viscous friction generated when the fluid flows through the gap, that is F = cV ,where α is an index between 0 and 1, when the fluid is Newtonian fluid,α = 1. The other is to achieve energy consumption by the pressure difference formed by the small orifice throttling on the piston, F = cV n , where n is dependent upon the velocity of flow, when the velocity of flow is low, that is approximately linear viscous damping, n = 1, when it is too high, it presents the squared characteristic, n = 2 [20].…”
Section: Damping Mechanism In Fluid Damping Isolatorsmentioning
confidence: 99%
“…Based on the comprehensive analysis, it is found that there are two main energy-consuming methods for fluid damping: One is the gap flow, which achieves the energy consumption by the viscous friction generated when the fluid flows through the gap, that is F = cV ,where α is an index between 0 and 1, when the fluid is Newtonian fluid,α = 1. The other is to achieve energy consumption by the pressure difference formed by the small orifice throttling on the piston, F = cV n , where n is dependent upon the velocity of flow, when the velocity of flow is low, that is approximately linear viscous damping, n = 1, when it is too high, it presents the squared characteristic, n = 2 [20].…”
Section: Damping Mechanism In Fluid Damping Isolatorsmentioning
confidence: 99%
“…Silicon–carbon–fiber‐reinforced silicon carbide matrix composites (SiC f /SiC) are regarded as one of the most promising materials for aircraft hot section components due to their excellent mechanical properties in high‐temperature environments 1–9 . When assembling complex high‐temperature section components, ceramic–matrix composites (CMCs) joints with high mechanical properties are used to ensure the structural strength of the joint 10,11 .…”
Section: Introductionmentioning
confidence: 99%
“…Silicon-carbon-fiber-reinforced silicon carbide matrix composites (SiC f /SiC) are regarded as one of the most promising materials for aircraft hot section components due to their excellent mechanical properties in hightemperature environments. [1][2][3][4][5][6][7][8][9] When assembling complex high-temperature section components, ceramic-matrix composites (CMCs) joints with high mechanical properties are used to ensure the structural strength of the joint. 10,11 The 2D CMCs z-pinned joint is a mechanical joint with excellent performance, which could be widely used in the connection of complex aircraft thermal sections in the future.…”
Section: Introductionmentioning
confidence: 99%
“…Barriers to their successful application include the lack of knowledge of in situ damages of their constituent phases and the correlation of these damages to the final failure of the entire composites. Understanding the damage mechanism in the interphase between the fiber and matrix is one of the most important issues [5][6][7].…”
Section: Introductionmentioning
confidence: 99%