Guided Wave Sensitivity for De-Bond Defects in Aluminum Skin-Honeycomb Core
Sandwich plates are finding an increasing range of application in the aircraft industry. The inspection of honeycomb composite structure by conventional ultrasonic technique is complex and very time consuming. The present study demonstrates a technique using guided Lamb waves at low frequencies to predict de-bond defects in aluminum skin-honeycomb core sandwich structure used in aeronautics. The numerical method was investigated for drawing the dispersion and displacement curves of ultrasonic Lamb wave propagated in Aluminum plate. An experimental study was carried out to check the theoretical prediction. The detection of unsticking between the skin and the core was tested by the two first modes for a low frequency. It was found that A0 mode is more sensitive to delamination defect compared to S0 mode.
[1] Roman Ruzek, Radek Lohonka, Josef Jironc, Ultrasonic C-Scan and
shearography NDI techniques evaluation of impact defects
identification. NDT & E International 39 (2006) 132-142.
[2] S. Bourasseau, M. Dupont, D. Balageas, E. Bocherens, Impact damage
detection in radome sandwich structures by traditional non destructive
evaluation and fiber optic integrated health monitoring systems.10th
International Conference on Adaptive Structures and Technologies,
ICAS T499, Paris (France), October 11-13,1999.
[3] Kisoo Kang, Manyong Choi, Koungsuk Kim, Yonghum Cha,
Youngjune Kang, Inspection of impact damage in h honeycomb
composite plate by ESPI, ultrasonic testing and thermography, 12th APCNDT
2006-Asia-Pasific Conference on NDT, 5th-10th Nov 2006,
Auckland, New Zealand.
[4] N. Guo and P. Cawley, The interaction of Lamb waves with
delaminations in composite laminates, J.Acoust.Soc.Am.94 (4), October,
(1993) 2240-2246.
[5] Zhongqing Su, Lin Ye, Ye Lu. Guided Lamb waves for identification of
damage in composite structures, Journal of Sound and Vibration 295
(2006) 753-780.
[6] H.Duflo and al.I, Interaction of Lamb waves on bonded composite plates
with defects, Composite Structures 79 (2007) 229-233.
[7] A. Satour and F. Boubenider, Use of guided waves for inspection of
composite skin-Honeycomb core, Material science Forum. Vols 636-637
(2010), pp 1533-1540.
[8] Hay. T, Lou Wei and Rose J. L. Rapid Inspection of Composite Skin-
Honeycomb Core Structures with Ultrasonic Guided Waves, Journal of
Composite Materials, 2003, 37 (10): 929-939.
[9] A Victorov (1967), Rayleigh and Lamb waves, Plenum press, New
York.
[10] Royer, D. Dieulesaint, E, Ondes élastique dans les solides, Tome1,
propagation libre et guidée. Paris : Masson, 1996.p.308.
[11] K. Diamanti, C. Soutis, J. M. Hodgkinson, Lamb waves for the nondestructive
inspection of monolithic and sandwich composite beams,
Compositers: Part A36 (2005) 189-195.
[12] Guo N, Lim MK. In: Thompson DO, Chimenti DE, editors. Lamb waves
propagation in aluminum honeycomb structures. Review of progress in
quantitative nondestructive evaluation. New York: Plenum Press; 1996,
p.323-30.
[1] Roman Ruzek, Radek Lohonka, Josef Jironc, Ultrasonic C-Scan and
shearography NDI techniques evaluation of impact defects
identification. NDT & E International 39 (2006) 132-142.
[2] S. Bourasseau, M. Dupont, D. Balageas, E. Bocherens, Impact damage
detection in radome sandwich structures by traditional non destructive
evaluation and fiber optic integrated health monitoring systems.10th
International Conference on Adaptive Structures and Technologies,
ICAS T499, Paris (France), October 11-13,1999.
[3] Kisoo Kang, Manyong Choi, Koungsuk Kim, Yonghum Cha,
Youngjune Kang, Inspection of impact damage in h honeycomb
composite plate by ESPI, ultrasonic testing and thermography, 12th APCNDT
2006-Asia-Pasific Conference on NDT, 5th-10th Nov 2006,
Auckland, New Zealand.
[4] N. Guo and P. Cawley, The interaction of Lamb waves with
delaminations in composite laminates, J.Acoust.Soc.Am.94 (4), October,
(1993) 2240-2246.
[5] Zhongqing Su, Lin Ye, Ye Lu. Guided Lamb waves for identification of
damage in composite structures, Journal of Sound and Vibration 295
(2006) 753-780.
[6] H.Duflo and al.I, Interaction of Lamb waves on bonded composite plates
with defects, Composite Structures 79 (2007) 229-233.
[7] A. Satour and F. Boubenider, Use of guided waves for inspection of
composite skin-Honeycomb core, Material science Forum. Vols 636-637
(2010), pp 1533-1540.
[8] Hay. T, Lou Wei and Rose J. L. Rapid Inspection of Composite Skin-
Honeycomb Core Structures with Ultrasonic Guided Waves, Journal of
Composite Materials, 2003, 37 (10): 929-939.
[9] A Victorov (1967), Rayleigh and Lamb waves, Plenum press, New
York.
[10] Royer, D. Dieulesaint, E, Ondes élastique dans les solides, Tome1,
propagation libre et guidée. Paris : Masson, 1996.p.308.
[11] K. Diamanti, C. Soutis, J. M. Hodgkinson, Lamb waves for the nondestructive
inspection of monolithic and sandwich composite beams,
Compositers: Part A36 (2005) 189-195.
[12] Guo N, Lim MK. In: Thompson DO, Chimenti DE, editors. Lamb waves
propagation in aluminum honeycomb structures. Review of progress in
quantitative nondestructive evaluation. New York: Plenum Press; 1996,
p.323-30.
@article{"International Journal of Engineering, Mathematical and Physical Sciences:65165", author = "A. Satour and F. Boubenider and R. Halimi and A. Badidibouda", title = "Guided Wave Sensitivity for De-Bond Defects in Aluminum Skin-Honeycomb Core", abstract = "Sandwich plates are finding an increasing range of application in the aircraft industry. The inspection of honeycomb composite structure by conventional ultrasonic technique is complex and very time consuming. The present study demonstrates a technique using guided Lamb waves at low frequencies to predict de-bond defects in aluminum skin-honeycomb core sandwich structure used in aeronautics. The numerical method was investigated for drawing the dispersion and displacement curves of ultrasonic Lamb wave propagated in Aluminum plate. An experimental study was carried out to check the theoretical prediction. The detection of unsticking between the skin and the core was tested by the two first modes for a low frequency. It was found that A0 mode is more sensitive to delamination defect compared to S0 mode.
", keywords = "Damage detection, delamination, guided waves, Sandwich structure. ", volume = "7", number = "9", pages = "1451-4", }
