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Monitoring Damage Accumulation in Continuous Fiber-Reinforced Ceramic-Matrix Composites with Different Fiber Preforms under Cyclic Loading Using Hysteresis-Based Damage Parameters
Li Longbiao
College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, No.29 Yudao St., Nanjing 210016, PR China
received February 1, 2018, received in revised form February 12, 2018, accepted February 22, 2018
Vol. 9, No. 3, Pages 235-262 DOI: 10.4416/JCST2018-00010
Abstract
In this paper, the damage accumulation of continuous fiber-reinforced ceramic-matrix composites (CMCs) with different fiber preforms, i.e. 2D and 2.5D woven, 3D braided and needled C/SiC, 2D and 3D woven SiC/SiC composites, subject to cyclic tensile loading/unloading at room temperature has been investigated using the hysteresis-based damage parameters. Based on the damage mechanisms of matrix multiple cracking modes and relative frictional sliding between fibers and the matrix, the relationships between the hysteresis-based damage parameters and damage mechanisms of matrix cracking modes, fiber/matrix interface debonding/sliding have been established. The cyclic tensile loading/unloading stress/strain hysteresis loops, matrix cracking mode ratio and fiber/matrix interface sliding ratio of 2D and 2.5D woven, 3D braided and needled C/SiC, and 2D and 3D woven SiC/SiC composites have been predicted for different peak stresses. The comparisons of damage accumulation between C/SiC and SiC/SiC composites with different fiber preforms under cyclic tensile loading/unloading have been analyzed.
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Keywords
Ceramic-matrix composites (CMCs), damage accumulation, matrix cracking, interface debonding, hysteresis loops.
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