Degradation in mechanical properties (compression, flexural and ILS) of glass epoxy composite laminates with induced defects (simulating delaminations) was studied. The defects were characterized by using the A-scan ultrasonic pulse-echo technique. The two A-scan parameters, viz. the back wall echo amplitude and time of flight, were followed respectively, as functions of the defect size (diameter) and its location in the laminate thickness. The mechanical properties of laminates were evaluated destructively for different defect sizes and locations. An attempt has been made to express the mechanical properties in terms of the two NDT scan parameters characterizing the defects and empirical equations presented.
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Arulmurugan Coll Engn, Dept Mech Engn, Karur, Tamil Nadu, India
Anna Univ, Dept Mech Engn, Madras 600025, Tamil Nadu, IndiaArulmurugan Coll Engn, Dept Mech Engn, Karur, Tamil Nadu, India
Vivekanandhan, Chinnasamy
Sampath, Pavayee Subramani
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KSR Coll Technol, Dept Mech Engn Coll, Tiruchengode, Tamil Nadu, IndiaArulmurugan Coll Engn, Dept Mech Engn, Karur, Tamil Nadu, India
机构:
Dept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, AustraliaDept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, Australia
Tan, P.
Tong, L.
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Dept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, AustraliaDept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, Australia
Tong, L.
Steven, G.P.
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Dept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, AustraliaDept. of Aeronautical Engineering, University of Sydney, Sydney, NSW 2006, Australia