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    An Investigation of the End-Notched Flexure and End-Loaded Split Tests Applied to the Mode II Interlaminar Fracture of a SiC/SiC Ceramic Matrix Composite

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 004
    Author:
    Presby, Michael J.
    ,
    Kannan, Manigandan
    ,
    Morscher, Gregory N.
    ,
    Godines, Cody
    ,
    Eftekharian, Amirhossein
    ,
    Ahmad, Jalees
    ,
    Abdi, Frank
    ,
    Choi, Sung R.
    DOI: 10.1115/1.4044490
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Delamination is a common failure mode observed in ceramic matrix composites (CMCs) and occurs as a result of applied interlaminar tensile and shear stresses exceeding the interlaminar strength. As CMCs are further implemented into aero engines, the need to understand their interlaminar failure becomes increasingly important. While significant contributions have been made toward understanding the mode I fracture toughness of CMCs, limited work exists on mode II. Several test methods for measuring the mode II fracture toughness have been proposed in the literature, namely, the end-notched flexure (ENF) and the end-loaded split (ELS) tests. This work investigates the mode II fracture toughness of a melt-infiltrated SiC/SiC CMC at ambient temperature using the ENF and ELS test methods. Acoustic emission (AE), direct current potential drop (DCPD), and digital image correlation (DIC) are implemented as health monitoring techniques to monitor crack initiation and propagation. Results show reasonable correlation between the two test methods and that the ELS test method is better suited for characterizing R-curve behavior.
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      An Investigation of the End-Notched Flexure and End-Loaded Split Tests Applied to the Mode II Interlaminar Fracture of a SiC/SiC Ceramic Matrix Composite

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4274187
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorPresby, Michael J.
    contributor authorKannan, Manigandan
    contributor authorMorscher, Gregory N.
    contributor authorGodines, Cody
    contributor authorEftekharian, Amirhossein
    contributor authorAhmad, Jalees
    contributor authorAbdi, Frank
    contributor authorChoi, Sung R.
    date accessioned2022-02-04T14:41:54Z
    date available2022-02-04T14:41:54Z
    date copyright2020/02/18/
    date issued2020
    identifier issn0742-4795
    identifier othergtp_142_04_041027.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274187
    description abstractDelamination is a common failure mode observed in ceramic matrix composites (CMCs) and occurs as a result of applied interlaminar tensile and shear stresses exceeding the interlaminar strength. As CMCs are further implemented into aero engines, the need to understand their interlaminar failure becomes increasingly important. While significant contributions have been made toward understanding the mode I fracture toughness of CMCs, limited work exists on mode II. Several test methods for measuring the mode II fracture toughness have been proposed in the literature, namely, the end-notched flexure (ENF) and the end-loaded split (ELS) tests. This work investigates the mode II fracture toughness of a melt-infiltrated SiC/SiC CMC at ambient temperature using the ENF and ELS test methods. Acoustic emission (AE), direct current potential drop (DCPD), and digital image correlation (DIC) are implemented as health monitoring techniques to monitor crack initiation and propagation. Results show reasonable correlation between the two test methods and that the ELS test method is better suited for characterizing R-curve behavior.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Investigation of the End-Notched Flexure and End-Loaded Split Tests Applied to the Mode II Interlaminar Fracture of a SiC/SiC Ceramic Matrix Composite
    typeJournal Paper
    journal volume142
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4044490
    page41027
    treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 004
    contenttypeFulltext
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