Volume 1: Advances in Aerospace Technology 2014
DOI: 10.1115/imece2014-36583
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Effective Mechanical Properties of Carbon-Carbon Composites

Abstract: In recent times, composite materials have gained mainstream acceptance as a structural material of choice due to their tailorability and improved thermal, specific strength/stiffness and durability performance [1–3]. For high temperature applications, which include exit nozzle for rockets, leading edge for missiles, nose cones, brake pads etc. Carbon-Carbon composites (C/C composite) are found suitable [4–6]. Mechanical property estimation of C/C composites is challenging due to their highly heterogeneous micr… Show more

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Cited by 5 publications
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“…Quantities with a prime are associated with R 0 . The displacement components (u, v, w) in the respective (x, y, z) directions obey the constraint equations (faces) as follows 12,27…”
Section: Declaration Of Conflicting Interestsmentioning
confidence: 99%
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“…Quantities with a prime are associated with R 0 . The displacement components (u, v, w) in the respective (x, y, z) directions obey the constraint equations (faces) as follows 12,27…”
Section: Declaration Of Conflicting Interestsmentioning
confidence: 99%
“…3,[8][9][10][11] However, the assumptions used for analytical model development prevent them from predicting material behavior by considering actual micro-structure of FRPs in addition to accounting for different damage mechanisms. 12 On the other hand, empirical models are inadequate in terms of capturing the physics of the damage mechanisms and often times, fail to yield accurate predictions. 13 Additionally, unlike macro-scale experiments, 14,15 conducting microscale experiments to capture micro-scale damage mechanisms in FRPs is quite complex and difficult to carry out.…”
Section: Introductionmentioning
confidence: 99%
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