Inverse heat transfer approach for nondestructive estimation the size and depth of subsurface defects of CFRP composite using lock-in thermography

被引:24
作者
Gong Jinlong
Liu Junyan [1 ]
Wang Fei
Wang Yang [1 ]
机构
[1] Harbin Inst Technol, Sch Mechatron Engn, Harbin 150001, Peoples R China
关键词
Inverse heat transfer problem; Lock-in thermography; Subsurface defect; Hybrid method; AIRCRAFT COMPOSITES; IMPACT DAMAGE;
D O I
10.1016/j.infrared.2015.06.005
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
An inverse heat transfer approach is developed to characterize the size and depth of subsurface defects in CFRP composite materials through the reconstruction phase profile of lock-in thermography (LIT) obtained by finite element simulation. This work mainly focuses on the application of hybrid method that integrates simulation annealing algorithm (SA) and Nelder-Mead simplex search method (NM) for determination of the sizes and depths of subsurface defects within the CFRP laminate materials. For this purpose, an 808 nm laser is used for imposing a modulated heat excitation on the CFRP laminate specimen, and the thermal images are collected using an infrared camera. The hybrid method is employed to find the optimal solutions of the objective or cost function constructed by phase profile of LIT between an experimental configuration and numerical solution for a CFRP specimen. The experimental results show that the size and depth of subsurface defects are effectively obtained through inverse solving the constructed objective or cost function by the hybrid method. The estimated maximum errors for the size and depth are less than 5% and 4% for given subsurface defects by the proposed method, respectively. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:439 / 447
页数:9
相关论文
共 20 条
[1]  
ABQUS Software, 2012, ABQUS SOFTW VERS 201
[2]  
Almond D., 1996, PHOTOTHERMAL SCI TEC
[3]   Aircraft composites assessment by means of transient thermal NDT [J].
Avdelidis, NP ;
Almond, DP ;
Dobbinson, A ;
Hawtin, BC ;
Ibarra-Castanedo, C ;
Maldague, X .
PROGRESS IN AEROSPACE SCIENCES, 2004, 40 (03) :143-162
[4]   The detection and measurement of impact damage in thick carbon fibre reinforced laminates by transient thermography [J].
Ball, RJ ;
Almond, DP .
NDT & E INTERNATIONAL, 1998, 31 (03) :165-173
[5]   THERMAL WAVE IMAGING WITH PHASE SENSITIVE MODULATED THERMOGRAPHY [J].
BUSSE, G ;
WU, D ;
KARPEN, W .
JOURNAL OF APPLIED PHYSICS, 1992, 71 (08) :3962-3965
[6]   Defect detection in aircraft composites by using a neural approach in the analysis of thermographic images [J].
D'Orazio, T ;
Guaragnella, C ;
Leo, M ;
Spagnolo, P .
NDT & E INTERNATIONAL, 2005, 38 (08) :665-673
[7]   A genetic algorithm and a particle swarm optimizer hybridized with Nelder-Mead simplex search [J].
Fan, Shu-kai S. ;
Liang, Yun-Chia ;
Zahara, Erwie .
COMPUTERS & INDUSTRIAL ENGINEERING, 2006, 50 (04) :401-425
[8]  
Hanke M., 2017, Conjugate Gradient Type Methods for ill-Posed Problems
[9]   Thermal characterization of anisotropic media in photothermal point, line, and grating configuration [J].
Kalogiannakis, G. ;
Van Hemelrijck, D. ;
Longuemart, S. ;
Ravi, J. ;
Okasha, A. ;
Glorieux, C. .
JOURNAL OF APPLIED PHYSICS, 2006, 100 (06)
[10]   Research on the quantitative analysis of subsurface defects for non-destructive testing by lock-in thermography [J].
Liu Junyan ;
Tang Qingju ;
Liu Xun ;
Wang Yang .
NDT & E INTERNATIONAL, 2012, 45 (01) :104-110