TY - JOUR
T1 - Mechanical behaviour of ±55° filament-wound glass-fibre/epoxy-resin tubes - III. Macromechanical model of the macroscopic behaviour of tubular structures with damage and failure envelope prediction
AU - Hu, Gengkai
AU - Bai, Jinbo
AU - Demianouchko, Ekaterina
AU - Bompard, Philippe
PY - 1998
Y1 - 1998
N2 - This series of papers on ±55° filament-wound glass-fibre/ epoxy-resin tubes consists of three parts. In the present paper (Part III), the macroscopic mechanical behaviour of the tubular structure is presented. A method for predicting composite tube macroscopic properties from the ply constants is given. A more general analytical method is used for determining ply stresses of a composite tube under a combined load, which will then be compared with 3D finite-element analysis, classical and adjusted laminate theory. Failure envelope prediction is then made according to the micro- and meso-scale model results. The stresses distribution in the tube thickness direction predicted by the present method agrees well with 3D finite-element analyses. Four methods give similar stress distribution results under tensile loading, but different ones under internal pressure loading. For failure envelope prediction, the first-ply-failure theory underestimates the failure load for pressure dominated loading. The effect of possible micro structural damage on the failure load prediction is also discussed and compared with experimental results. In Part I (Bai et al. Compos. Sci. Technol., 1997, 57, 141-153), the microstructure, mechanical behaviour and damage initiation mechanisms were presented. In Part II (Bai et al. Compos. Sci. Technol., 1997, 57, 155-164), micrornechanical modelling of the damage initiation was conducted in order to determine the mechanical conditions under which different microcracking mechanisms occur.
AB - This series of papers on ±55° filament-wound glass-fibre/ epoxy-resin tubes consists of three parts. In the present paper (Part III), the macroscopic mechanical behaviour of the tubular structure is presented. A method for predicting composite tube macroscopic properties from the ply constants is given. A more general analytical method is used for determining ply stresses of a composite tube under a combined load, which will then be compared with 3D finite-element analysis, classical and adjusted laminate theory. Failure envelope prediction is then made according to the micro- and meso-scale model results. The stresses distribution in the tube thickness direction predicted by the present method agrees well with 3D finite-element analyses. Four methods give similar stress distribution results under tensile loading, but different ones under internal pressure loading. For failure envelope prediction, the first-ply-failure theory underestimates the failure load for pressure dominated loading. The effect of possible micro structural damage on the failure load prediction is also discussed and compared with experimental results. In Part I (Bai et al. Compos. Sci. Technol., 1997, 57, 141-153), the microstructure, mechanical behaviour and damage initiation mechanisms were presented. In Part II (Bai et al. Compos. Sci. Technol., 1997, 57, 155-164), micrornechanical modelling of the damage initiation was conducted in order to determine the mechanical conditions under which different microcracking mechanisms occur.
KW - Delamination
KW - Failure criterion
KW - Meso and macromechanical modelling
KW - Stress analysis
KW - Transverse cracking
UR - http://www.scopus.com/inward/record.url?scp=23044481979&partnerID=8YFLogxK
U2 - 10.1016/S0266-3538(97)00078-X
DO - 10.1016/S0266-3538(97)00078-X
M3 - Article
AN - SCOPUS:23044481979
SN - 0266-3538
VL - 58
SP - 19
EP - 29
JO - Composites Science and Technology
JF - Composites Science and Technology
IS - 1
ER -