Accession Number:

ADA614883

Title:

Characterization of the Effect of Fiber Undulation on Strength and Stiffness of Composite Laminates

Descriptive Note:

Final rept. 15 May-20 Aug 2013

Corporate Author:

ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD VEHICLE TECHNOLOGY DIRECTORATE

Report Date:

2015-03-01

Pagination or Media Count:

28.0

Abstract:

Stiffness and strength predictions of undulated composites filament-wound cylinders, braids, plain weaves, etc. using traditional laminated composite theories are complicated by complex fiber architecture. Undulations consisting of fibers passing over and under each other result from the interweaving process. In the current investigation, full-field strain measurements were used to evaluate local strain distributions in the region of a 0 undulated ply in a 0n90ns laminate n 2,4,6 and a 30 undulated ply in a 30n 60ns laminate n 2,4. Specimens were manufactured with carbon fibers, various amplitudes of undulation, and matrix materials with moduli ranging from 300 to 3,000 MPa. Two-dimensional digital image correlation was used on the free edges of the compressively loaded specimens. The observed strain fields were highly influenced by the undulation geometry. The axial modulus Ex of a 0n90ns laminate was more sensitive to reinforcement undulation for flexible matrixes 300 MPa rather than rigid 3,000 MPa. Fiber undulation was observed to elevate out-of-plane shear and through-thickness normal strains in regions eventually involved in the fiber microbuckling failure process.

Subject Categories:

  • Laminates and Composite Materials
  • Machinery and Tools
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE