4.4 Article

Effects of Constituents and Lay-up Configuration on Drop-Weight Tests of Fiber-Metal Laminates

Journal

APPLIED COMPOSITE MATERIALS
Volume 17, Issue 1, Pages 43-62

Publisher

SPRINGER
DOI: 10.1007/s10443-009-9119-1

Keywords

Drop-weight (low-velocity) impact; Fiber-metal laminates (GLARE and ARALL); Ultrasound

Funding

  1. NASA [NAG3-2259]
  2. PSC-CUNY [61429-00 30, 62466-00 31]
  3. Army Research Office [DAAD19-99-1-0366]

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Impact responses and damage of various fiber-metal laminates were studied using a drop-weight instrument with the post-impact damage characteristics being evaluated through ultrasonic and mechanical sectioning techniques. The first severe failure induced by the low-velocity drop-weight impact occurred as delamination between the aluminum and fiber-epoxy layers at the non-impact side. It was followed by a visible shear crack in the outer aluminum layer on the non-impact face. Through-thickness shear cracks in the aluminum sheets and severe damage in the fiber laminated layers (including delamination between adjacent fiber-epoxy laminae with different fiber orientations) developed under higher energy impacts. The impact properties of fiber-metal laminates varied with different constituent materials and fiber orientations. Since it was punched through easily, the aramid-fiber reinforced fiber-metal laminates (ARALL) offered poorer impact resistance than the glass-fiber reinforced fiber-metal laminates (GLARE). Tougher and more ductile aluminum alloys improved the impact resistance. GLARE made of cross-ply prepregs provided better impact resistance than GLARE with unidirectional plies.

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