Effect of compression and tension types of concentrated edge loads on buckling and vibration behavior of interlaminar hybrid fibre metal laminates

Author:

Muddappa P.P. Yathish,Rajanna T.,Giridhara G.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference43 articles.

1. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J. Mater. Process. Technol.,2000

2. Fiber/metal composite technology for future primary aircraft structures;Alderliesten;J. Aircr.,2008

3. ARALL: A materials challenge for the next generation of aircraft;Vogelesang;Mater. Des.,1986

4. Towards technology readiness of fibre: Glare Technology Development (GTO) 1997-2000;Gunnink,2000

5. Impact resistance of fiber-metal laminates: a review;Sadighi;Int. J. Impact Eng.,2012

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