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Low-Velocity Impact Behavior of Aluminum-Fiber/Epoxy Laminates: A Comprehensive Experimental Study

[+] Author Affiliations
Mohammad Alemi-Ardakani, Abbas S. Milani

University of British Columbia Okanagan, Kelowna, BC, Canada

Akbar Afaghi-Khatibi

University of Tehran, Tehran, Iran

Hady Parsaiyan

Amirkabir University of Technology, Tehran, Iran

Paper No. DETC2010-28731, pp. 59-68; 10 pages
doi:10.1115/DETC2010-28731
From:
  • ASME 2010 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
  • Volume 1: 36th Design Automation Conference, Parts A and B
  • Montreal, Quebec, Canada, August 15–18, 2010
  • Conference Sponsors: Design Engineering Division and Computers in Engineering Division
  • ISBN: 978-0-7918-4409-0 | eISBN: 978-0-7918-3881-5
  • Copyright © 2010 by ASME

abstract

Considering many potential applications of fiber reinforced metal laminates (FMLs) in sensitive structures, it is necessary to understand their mechanical behavior under impact loads. In this study, low velocity impact tests based on ASTM D7136 have been conducted on FMLs made of 1050 aluminum sheets and various types of fiber reinforced polymer (FRP) layers; namely E-Glass, Kevlar 49, and carbon T300 plain woven in the epoxy resin. Projectile energy, fiber type and the number of successive impacts are selected among important parameters that can affect the performance of FMLs. In particular, the effects of these parameters on the absorbed energy, contact force, front and rear face damage areas, central deflection and permanent deformation of FMLs have been investigated. For determining the damage area and central deflection of the specimens, an image processing method is adapted.

Copyright © 2010 by ASME

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