Contact Behaviour of Composite Laminate under Quasi-Static Indentation Load
نویسندگان
چکیده
منابع مشابه
Contact Behaviour of Composite Laminate under Quasi-Static Indentation Load
A viable solution to the ever-demanding weight-saving target in aerospace industry is the replacement of conventional engineering alloys with composite materials in primary structures. A major concern to the effective use of composite laminates is the substantial reduction in the compressive strength when the contact force has exceeded the delamination threshold load (DTL). This paper focuses o...
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ژورنال
عنوان ژورنال: Key Engineering Materials
سال: 2013
ISSN: 1662-9795
DOI: 10.4028/www.scientific.net/kem.577-578.545