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dc.contributor.authorMattison, Jacob T.
dc.contributor.authorFaucett, D. Calvin
dc.contributor.authorChoi, Sung R.
dc.date.accessioned2025-04-21T10:12:57Z
dc.date.available2025-04-21T10:12:57Z
dc.date.copyright9/13/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0742-4795
dc.identifier.othergtp_147_01_011008.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305726
dc.description.abstractThis paper was to present how an affordable, high-temperature, interlaminar tension (ILT) strength testing method was explored and developed for ceramic matrix composites (CMCs), leading to development of a diametral-compression test methodology. The test methodology was first delved and verified at ambient temperature by employing a model, 2D-woven polymer matrix composite (PMC) with various test-specimen configurations. The test method was then applied to and confirmed with two different gas-turbine grade CMCs of 2D melt-infiltrated (MI) SiC/SiC and 2D N720/alumina oxide/oxide at both ambient and elevated temperatures. Life prediction testing was also conducted at 1316 °C for the MI SiC/SiC to validate the effectiveness of test method for a long-term life prediction testing. All of the results on strength and life prediction testing indicated an applicability and feasibility as an appropriate high-temperature ILT test methodology in CMCs with provisions of simplicity, affordability, and technical soundness.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleDevelopment of High-Temperature, Interlaminar Tension Test Methodology for Ceramic Matrix Composites
dc.typeJournal Paper
dc.journal.volume147
dc.journal.issue1
dc.journal.titleJournal of Engineering for Gas Turbines and Power
dc.identifier.doi10.1115/1.4066288
dc.journal.fristpage11008-1
dc.journal.lastpage11008-8
dc.page8
dc.treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 001
dc.contenttypeFulltext


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