Progressive damage modelling of bonded composite repairs

被引:68
作者
Papanikos, P
Tserpes, KI
Labeas, G
Pantelakis, S
机构
[1] ISTRAM, Patras 26441, Greece
[2] Univ Patras, Dept Mech Engn & Aeronaut, Lab Technol & Strength Mat, Patras 36500, Greece
关键词
progressive damage; bonded repair; composite; finite element; air frame;
D O I
10.1016/j.tafmec.2005.01.004
中图分类号
TH [机械、仪表工业];
学科分类号
0802 [机械工程];
摘要
Presented is a three-dimensional progressive damage model that can assess the mechanical behaviour of bonded composite repairs of cracked metallic plates. The model is able to assess the stress intensity factor (SIF) at the crack tip, patch debonding and damage accumulation in the composite patch as functions of the applied load. Considered are the stress analysis, failure analysis and material property degradation. Stress analysis is performed using a three-dimensional detailed parametric finite element (FE) model developed using the ANSYS FE code. Failure analysis is performed using a set of stress-based polynomial failure criteria. Material property degradation of the failed material (patch and adhesive) is performed using appropriate degradation rules. The three model components have been programmed in the ANSYS FE code creating a user-friendly parametric macro-routine, which can be easily applied to bonded repairs of different materials and configuration. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:189 / 198
页数:10
相关论文
共 18 条
[1]
[Anonymous], 2002, ANSYS US MAN VERS 6
[3]
Callinan RJ, 1997, ADVANCES IN FRACTURE RESEARCH, VOLS 1-6, P2151
[4]
ANALYTICAL ESTIMATION OF STRESS INTENSITY FACTORS IN PATCHED CRACKED PLATES [J].
CHANDRA, R ;
MURTHY, MVV ;
RAMAMURTHY, TS ;
RAO, AK .
ENGINEERING FRACTURE MECHANICS, 1985, 21 (03) :479-494
[5]
FINITE-ELEMENT ANALYSIS OF PATCHED CRACKS [J].
JONES, R ;
CALLINAN, RJ .
JOURNAL OF STRUCTURAL MECHANICS, 1979, 7 (02) :107-130
[6]
Kumar AR, 2000, COMPOS STRUCT, V49, P285
[7]
ANALYSIS OF COMPOSITE-REINFORCED CUTOUTS AND CRACKS [J].
MITCHELL, RA ;
WOOLLEY, RM ;
CHWIRUT, DJ .
AIAA JOURNAL, 1975, 13 (06) :744-749
[8]
Nonlinear analysis of bonded composite patch repair of cracked aluminum panels [J].
Naboulsi, S ;
Mall, S .
COMPOSITE STRUCTURES, 1998, 41 (3-4) :303-313
[9]
Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches [J].
Naboulsi, S ;
Mall, S .
THEORETICAL AND APPLIED FRACTURE MECHANICS, 1997, 28 (01) :13-28
[10]
Modeling of a cracked metallic structure with bonded composite patch using the three layer technique [J].
Naboulsi, S ;
Mall, S .
COMPOSITE STRUCTURES, 1996, 35 (03) :295-308