journal article·2016-05

Fatigue characterization of Poly Vinyl Chloride (PVC) foam core sandwich composite using the G-control method

Marcello Manca, Christian Berggreen, Leif A Carlsson, Pietro Bortolotti

Publisher page

Abstract

This paper presents experimental results from cyclic crack propagation tests performed on sandwich specimens with glass/epoxy face sheets and Poly Vinyl Chloride (PVC) foam cores using the G-controlled cyclic energy release rate (ΔG) test procedure. The face material was tested in tension, compression and shear to determine in-plane and out-of-plane mechanical properties, such as Young’s modulus, Poisson’s ratio and shear modulus. These properties were then used in an analytical model of the mixed-mode bending sandwich specimen to calculate compliance and energy release rate. Finite element analysis was used to determine the mode-mixity of the crack loading. Experimental crack growth cyclic tests were carried out on pre-cracked mixed-mode bending sandwich specimens with H45, H100 and H160 PVC foam cores under two mode-mixities (mode I and mode II dominant). Post-mortem analysis was performed on tested specimens, highlighting the influence of mode mixity and foam density on the crack path. Crack propagation diagrams showing da/dN versus ΔG curves were obtained to establish the Paris-Erdogan relation for each material combination tested at the two mode-mixities. Results showed constant crack growth rates for all the materials tested and revealed the influence on mode-mixity on crack propagation speed and foam density (higher foam density, slower crack propagation).
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Analysis of Composite Materials · Cellular and Composite Structures

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Mechanical Engineering, Technical University of Denmark, Lyngby, Denmark

Department of Ocean and Mechanical Engineering, Florida Atlantic University, FL, Boca Raton, USA

References (22)

Show source-provided references
1. 10.1046/j.1460-2695.1999.00148.x10.1046/j.1460-2695.1999.00148.x ↗
2. 10.1016/S0142-1123(01)00010-X10.1016/S0142-1123(01)00010-X ↗
3. 10.1016/j.compstruct.2012.05.02110.1016/j.compstruct.2012.05.021 ↗
4. 10.1016/j.compositesa.2012.07.00110.1016/j.compositesa.2012.07.001 ↗
5. 10.1177/109963621350530410.1177/1099636213505304 ↗
6. Manca M, Berggreen C and Carlsson LA. G-control fatigue testing for cyclic crack propagation in composite structures. Eng Fract Mech 2015. DOI: 10.1016/j.engfracmech.2015.06.059.10.1016/j.engfracmech.2015.06.059 ↗
7. MTS System Corporation, 2015, http://www.mts.com/testsuite/.
8. ASTM D3039 · 2014
9. ASTM D6641. Standard test method for compressive properties of polymer matrix composite materials using a combined loading compression (CLC) test fixture . West Conshohocken, PA; American Society for Testing and Materials, 2009.
10. ASTM D7078 · 2005
11. 10.1201/b1661810.1201/b16618 ↗
12. DIAB. Technical Manual . Divinycell H, Laholm, Sweden, 2014.
13. ASTM D6671/D6671-M-13 · 2013
14. Silversides I, Maslouhi A, Azzi M, et al. Delamination onset detection by AE monitoring in CFRP composites under quasi-static and cyclic loading. In: 26th annual technical conference of the American Society for Composites 2011 and the 2nd joint US-Canada conference on composites , Vol. 1, 2011, pp.573-592.
15. 10.1177/07316844950140080310.1177/073168449501400803 ↗
16. Berggreen C, Carlsson LA and Quispitupa A. Fatigue debond growth in sandwich structures loaded in mixed mode bending. In: Proceedings of the 13th European on Composite Materials , 2008.
17. 10.1177/109963620910453310.1177/1099636209104533 ↗
18. 10.1111/j.1460-2695.2011.01551.x10.1111/j.1460-2695.2011.01551.x ↗
19. 10.1016/j.engfracmech.2008.12.00810.1016/j.engfracmech.2008.12.008 ↗
20. 10.1177/002199830606528510.1177/0021998306065285 ↗
21. 10.1115/1.365690010.1115/1.3656900 ↗
22. 10.1016/j.engfracmech.2012.10.00910.1016/j.engfracmech.2012.10.009 ↗