Face/core debond fatigue crack growth characterization using the sandwich mixed mode bending specimen

被引:35
作者
Manca, Marcello [1 ]
Quispitupa, Amilcar [1 ]
Berggreen, Christian [1 ]
Carlsson, Leif A. [2 ]
机构
[1] Tech Univ Denmark, Dept Mech Engn, DK-2800 Lyngby, Denmark
[2] Florida Atlantic Univ, Dept Ocean & Mech Engn, Boca Raton, FL 33431 USA
关键词
Foams; Debonding; Interface; Fracture toughness; DAMAGE TOLERANCE; FRACTURE; INTERFACES;
D O I
10.1016/j.compositesa.2012.07.001
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Face/core fatigue crack growth in foam-cored sandwich composites is examined using the mixed mode bending (MMB) test method. The mixed mode loading at the debond crack tip is controlled by changing the load application point in the MMB test fixture. Sandwich specimens were manufactured using H45 and H100 PVC foam cores and E-glass/polyester face sheets. All specimens were pre-cracked in order to define a sharp crack front. The static debond fracture toughness for each material configuration was measured at different mode-mixity phase angles. Fatigue tests were performed at 80% of the static critical load, at load ratios of R = 0.1 and 0.2. The crack length was determined during fatigue testing using the analytical compliance expression and verified by visual measurements. Fatigue crack growth results revealed higher crack growth rates for mode I dominated loading. For specimens with H45 core, the crack grew just below the face/core interface on the core side for all mode-mixities, whereas for specimens with H100 core, the crack propagated in the core or in the face laminate depending on the mode-mixity at the debond crack tip. (c) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2120 / 2127
页数:8
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