Numerical Analys is of De fects in FML using Through - Transmission Mode of Active Thermography
International Journal of Engineering Trends and Technology (IJETT) | |
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© 2012 by IJETT Journal | ||
Volume-3 Issue-3 |
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Year of Publication : 2012 | ||
Authors : S.Sundaravalli , M.C.Majumder , G.K.Vijayaraghavan |
Citation
S.Sundaravalli , M.C.Majumder , G.K.Vijayaraghavan. "Numerical Analys is of De fects in FML using Through - Transmission Mode of Active Thermography ". International Journal of Engineering Trends and Technology (IJETT). V3(3):437-447 May-Jun 2012. ISSN:2231-5381. www.ijettjournal.org. published by seventh sense research group
Abstract
The study mainly focuses to investigate the thermal response of defects such as delaminations and disbonds, and develop mathematical models using numerical results to obtain the optimum heat requirement and time to identify defects in GL ARE type of Fibre metal laminates (FML) under a through - transmission (TT) mode of step pulsed active thermography (SPAT) method in the type of nondestructive testing and evaluation (NDTE) technique. The influence of applied heat flux and time on various si zes and depth of defects in FML is analysed to investigate the thermal response through numerical simulations. A finite element method (FEM) is applied to simulate SPAT through ANSYS software based on 3D transient heat transfer principle with the assumptio n of TT mode of observation. The investigation shows that t he smaller and near - surface defects located at the thermal stimulant side respond with reduced thermal contrast and vice versa. Numerical results are analysed to provide the optimum heat requi rement and time to identify defects at the required MRTD even to identify defects which are not identified within the load conditions considered for the investigation s . Further, a comparative study concludes that the numerical approach based on SPAT u sing TT mode of observation could be utilized to derive mathematical models using numerical results to analyse defects present in FML effectively .
References
[1] Ad Vlot and Jan Willem Gunnink , “ Fibre Metal Laminates ” : An Introduction. Kluwer Academic Publishers. Springer Netherlands , 2001 .
[2] ANSYS , ANSYS Heat Transfer Manual for Release 10 , 20 05 .
[3] Avdelidis N. P and Almond D.P , “ Transient thermography as a through skin imaging technique for airc raft assembly Modelling and experimental results ” , Journal of Infrared Phys. Technol ., 2004 , Vol. 45. No. 2, pp. 103 - 114.
[4] Avdelidis N.P, Almond D.P, Dob binson A, Hawtin B.C, Ibarra - Castanedo C and Maldague X, “ Aircraft composites assessment by means of transient thermal NDT ”, Progress in Aerospace Sciences, 2004 , Vol. 40, pp 143 – 162.
[5] Fahr A, Chapman, Forsyth, Poon and Laliberté, “ Nondestructive evaluatio n methods for damage assessment in fiber - metal laminates ”, Polymer Composites , 2000 , Vol. 21. No. 4, pp. 568 – 75.
[6] Guillen and Can, “ The influence of cooling rate on the fracture properties of a thermoplastic - based FMLs ”, Journal reinforced plastics and comp osites , 2002 , Vol. 21. No. 8, pp. 749 - 772.
[7] Hagenbeek M, “ Characterisation of Fibre Metal Laminates under Thermo - mechanical Loadings ” . PhD thesis. Faculty of Aerospace Engineering , 2005 , Delft University of Technology , pp 224.
[8] H ing Cheng L and Halabe Udaya B, “ Finite Element Modeling for Infrared Thermography of GFRP Bridge Decks ”, AIP Conference Proceedings , 2008 , Vol. 975. No. 1, pp. 1381 - 1386.
[9] Ibarra - Castanedo C , Grinzato E , Marinetti S , Bison P , Genest M , Grenier M , Jean - Marc Piau, Bendada A and Maldagu e X, “ Recent progresses in the inspection of aerospace components by infrared thermography ” 17th World Conference on Nondestructive Testing , 2008 , Shanghai, China, pp.25 - 28.
[10] Ibarra - Castanedo1 P , Avdelidis N.P , Grinzato G , Paolo G , Sergio M , Claudiu P , Ab delhakim B and Maldague X , “ Delamination detection and impact damage assessment of GLARE by active thermography ”, International Journal of materials and Product Technology , 2011 , Vol. 41, pp. 5 - 16.
[11] Krishnapillai M , Jones R , Marshall I.H , Bannister M , and Rajic N , “ NDTE using pulse thermography: Numerical modeling of composite subsurface defects ”, J. Composite Structures , 2006 , Vol. 75, pp. 241 - 249.
[12] Lugin S and Netzelmann U, “ A defect shape reconstruction algorithm for pulsed thermography ”, NDT&E Internati onal volume , 2007 , Vol. 40, pp. 220 – 228.
[13] Mabrouki F , Genest M , Shi G and Fahr A , “ Numerical modeling for thermographic inspection of fibre metal laminates ”, J. NDT and E International , 2009 , Vol. 42, pp. 581 - 588.
[14] Maldague X , “ Theory and practice of infrare d technology for nondestructive testing ” Wiley - Interscience, New York . 453 – 525 , 2001 .
[15] Meola C , Givanni M.C , Squillace A and Vitiello A , “ Non - destructive evaluation of aerospace materials with lock - in thermography ” J. Engineering Failure Analysis , 2006 , Vo l. 13. No. 3, pp. 380 - 388.
[16] Mirela S , Ibrarra - Castanedo , Maldague X , Bendada A, Svaic S and Boras I, “ Pulse thermography applied on a complex structure sample: comparison and analysis of numerical and experimental results ”, IV conferencia Panamericana de EN D , Buenos Aires , 2007 .
[17] Muralidhar C and Arya N.K , “ Evaluation of defects in axisymmetric composite structures by thermography ”, NDT&E International , 1993 , Vol. 26. No. 4, pp. 198 - 193.
[18] Muzia G , Rdzawski Z.M , Rojek M , Stabik J and Wróbel G , “ Thermographic di agnosis of fatigue degradation of epoxy - glass composites ”, Journal of Achievements in Materials and Manufacturing Engineering , 2007 , Vol. 24. No. 2, pp. 123 - 126.
[19] Omar M , Hassan M, Saito K and Alloo R, “ IR self - referencing thermography for detection of in - d epth defects ” , Journal of Infrared Physics and Technology , 2005 , 46 (4), pp 283 - 289.
[20] Omar M , Haassan M , Donohue K , Saito K and Alloo R , “ Infrared thermography for inspecting the adhesion integrity of plastic welded joints ”, NDT and E International , 2006 , Vo l. 39, pp. 1 - 7.
[21] Peter linde , Jürgen pleitner , Henk de boer and Jos sinke , “ Numerical and experimental simulation of damage behaviour of fibre metal laminates ”, 24th international congress of the aeronautical sciences , ICAS 2004 .
[22] Qiaojian Huang , Regez Brad , Krishnaswamy and Sridhar , “ The influence of disbond defects on Lamb wave testing in GLARE composites ” Pr oceedings of the SPIE , 2010 , Vol. 7650, pp. 76502P - 76502P - 8.
[23] Saintey M B and Almond D P, “ Defect Sizing by Transient Thermography II: A Numerical Treatment ”, Journal of physics. D, Applied physics , 1995 , Vol. 28, pp. 2539 - 2546.
[24] Speer. and Es - Said. 2004. Ap plications of an aluminum – beryllium composite for structural aerospace components, Engineering Failure Analysis , Vol. 11. No. 6, pp. 895 – 902.
[25] Timothy B Roth and Ann M. Anderson , “ A Light Transmission Based Liquid Crystal Thermography System ,” Journal of Heat Transfer, 2008 , Vol. 30. No.1,
[26] Vageswar A, Balasubramaniam K, Krishnamurthy C.V , Jayakumar T and Raj B, “ Periscope in frared thermography for local wall thinning in tubes ” , NDT&E International, 2009 , 42 (4), pp 275 – 282.
[27] Vijayaraghavan G K , Majumder M.C and Ramachandran K.P , “ Quantitative Analysis of Delaminations in GRP Pipes Using Thermal NDTE Technique ”, Journal of Adva nced Research in Mechanical Engineering, 2010 , Vol. 1. No. 1, pp.60 - 68
Keyword
Step pulsed active thermography (SPAT), T hrough - transmission mode (TT), NDTE, FML, Delamination s , Disbonds, Finite element method , Thermal contrast.