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Title: Compression strengths of advanced composites from a novel mini-sandwich beam

Journal Article · · SAMPE Quarterly (Society of Aerospace Material and Process Engineers); (United States)
OSTI ID:5457967
;  [1]
  1. Univ. of Dayton, OH (United States)

The intrinsic compression strength of advanced composites is difficult to measure, as the results often depend on the loading geometry and test conditions. Slight variations in specimen geometry can result in an eccentricity of the applied load with consequent specimen buckling. Complex test fixtures and specimen geometries have therefore been developed to avoid such premature failure under compressive loading. In spite of this, there is a large variation in reported strengths for some composites (notably those of intermediate-modulus carbon fibers), and failure strains are also significantly lower than those of the individual filaments. To better approximate the intrinsic composite compressive strength, a novel symmetric mini-sandwich beam was designed for testing. The beam has a composite skin (of variable thickness) on both sides of a neat resin core (of same material as the composite matrix). Unidirectional mini-sandwich specimens of AS4 and S-glass fibers in an epoxy matrix and AS4 in a PEEK matrix were tested in direct axial compression and four-point flexure. Failure occurred predominantly in the specimen gage section, at composite stresses and strains substantially higher than observed in corresponding tests on all composite-coupons. This paper discusses the fabrication and testing of these beams and analyzes the resulting compressive data and failure modes.

OSTI ID:
5457967
Journal Information:
SAMPE Quarterly (Society of Aerospace Material and Process Engineers); (United States), Vol. 22:3; ISSN 0036-0821
Country of Publication:
United States
Language:
English