Damage mechanisms and the mechanical properties of a laminated 0/90 ceramic/matrix composite
Damage mechanisms and the mechanical properties of a laminated 0/90 ceramic/matrix composite
The tensile properties of a 0/90 laminated CAS matrix composite reinforced with Nicalon fibers have been measured. Some effects of notches have also been explored. Changes in modulus and permanent strain caused by matrix cracking have been measured and compared with available models. For this comparison, independent measurements have been made of the constituent properties and the residual stress. The ultimate tensile strength has also been measured and compared with a global load-sharing model. It is concluded that lower-bound matrix cracking models provide good predictability of the stresses at which various matrix cracking mechanisms first operate. Also, the ultimate tensile strength is found to be consistent with a global load-sharing model, based on the in situ strength properties of the fibers. Conversely, the evolution of matrix cracks at stresses above the lower bound has yet to be adequately modeled. In addition, a need is identified for improved models relating elastic properties and permanent strains to matrix crack spacing.
3321-3330
Beyerle, Douglas S.
8b5e2059-7fe5-4681-96eb-1151eb821fa2
Spearing, S. Mark
9e56a7b3-e0e8-47b1-a6b4-db676ed3c17a
Evans, Anthony G.
0e10b0ae-fd33-4b1c-a1cb-78579ef8e68b
1992
Beyerle, Douglas S.
8b5e2059-7fe5-4681-96eb-1151eb821fa2
Spearing, S. Mark
9e56a7b3-e0e8-47b1-a6b4-db676ed3c17a
Evans, Anthony G.
0e10b0ae-fd33-4b1c-a1cb-78579ef8e68b
Beyerle, Douglas S., Spearing, S. Mark and Evans, Anthony G.
(1992)
Damage mechanisms and the mechanical properties of a laminated 0/90 ceramic/matrix composite.
Journal of the American Ceramic Society, 72 (12), .
(doi:10.1111/j.1151-2916.1992.tb04428.x).
Abstract
The tensile properties of a 0/90 laminated CAS matrix composite reinforced with Nicalon fibers have been measured. Some effects of notches have also been explored. Changes in modulus and permanent strain caused by matrix cracking have been measured and compared with available models. For this comparison, independent measurements have been made of the constituent properties and the residual stress. The ultimate tensile strength has also been measured and compared with a global load-sharing model. It is concluded that lower-bound matrix cracking models provide good predictability of the stresses at which various matrix cracking mechanisms first operate. Also, the ultimate tensile strength is found to be consistent with a global load-sharing model, based on the in situ strength properties of the fibers. Conversely, the evolution of matrix cracks at stresses above the lower bound has yet to be adequately modeled. In addition, a need is identified for improved models relating elastic properties and permanent strains to matrix crack spacing.
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Published date: 1992
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Local EPrints ID: 22857
URI: http://eprints.soton.ac.uk/id/eprint/22857
ISSN: 0002-7820
PURE UUID: 0e849b3b-0e20-4805-9d8c-e55af4f4ffd3
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Date deposited: 30 Jan 2007
Last modified: 16 Mar 2024 03:37
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Author:
Douglas S. Beyerle
Author:
Anthony G. Evans
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