Fatigue analyst and crack growth on GLARE (Glass Laminate Aluminum Reinforce Epoxy)

Subject Areas : Creep, Fatigue and Fracture Mechanic

Farzad  Emamalizadeh ¹ (Department of Mechanical Engineering, Semnan Branch, Islamic Azad University, Semnan, Iran)
seyyed meysam  hoseini ² (Department of Mechanical Engineering, K.N.Toosi University of Technology, Tehran, Iran)
Mohamad Jafar  Ostad Ahmad Ghorabi ³ (Strategic Center for Energy and Sustainable Development, Semnan Branch, Islamic Azad University, Semnan, Iran)

Received: 2015-09-01 Accepted : 2015-10-02 Published : 2015-05-22

Keywords: Stress intensity factor, fiber metal laminates, Fatigue Crack Growth,

Abstract :

Glass Laminate Aluminum Reinforced Epoxy consist of three or more layers of Al alloy and fibers alternatively. Fatigue crack growth rates in notched fiber-metal laminates under constant amplitude fatigue loading were studied numerically and were compared with them in monolithic 2024-t3 Al alloy plates, it’s shown that the fatigue life of Glare is more longer than monolithic 2024-t3 Al alloy plate and crack growth rate in Glare panel remain constant mostly even when crack is long. stress intensity factor for given crack tip position is determined by a finite element method in ABAQUSE system.