TY - JOUR
T1 - Estimation of the damage patterns in notched laminates with embedded FBG sensors
AU - Takeda, N.
AU - Yashiro, S.
AU - Okabe, T.
N1 - Funding Information:
This work was performed as a part of the project of “Civil Aviation Fundamental Technology Program-Advanced Materials and Process Development for Next Generation Aircraft Structures” under the contract of NEDO (New Energy and Industrial Technology Development Organization) founded by METI (Ministry of Economy, Trade and Industry), Japan. One of the authors, S.Y. acknowledges support by the Ministry of Education, Culture, Sports, Science and Technology of Japan under Grant-in-Aid for Scientific Research (No. 16-10761).
PY - 2006/5
Y1 - 2006/5
N2 - This study proposes a new method to estimate the damage patterns of notched composite laminates as an inverse problem using the reflection spectrum of embedded Fiber Bragg Grating (FBG) sensors. The damage pattern near the notch is analyzed by a layer-wise finite element model with cohesive elements to represent various cracks. The reflection spectrum of the FBG sensor is then analyzed from the strain distribution obtained in the damage analysis. The damage pattern is optimized as an inverse problem based on the above analyses while the spectrum shape is adopted as the objective function. The damage pattern is expressed by the residual strength distribution of the cohesive elements in the estimation scheme. The applied strain is also estimated by the wavelength shift of the reflection spectrum. The damage pattern and the applied strain estimated from the measured spectrum are found to agree with the experimental results.
AB - This study proposes a new method to estimate the damage patterns of notched composite laminates as an inverse problem using the reflection spectrum of embedded Fiber Bragg Grating (FBG) sensors. The damage pattern near the notch is analyzed by a layer-wise finite element model with cohesive elements to represent various cracks. The reflection spectrum of the FBG sensor is then analyzed from the strain distribution obtained in the damage analysis. The damage pattern is optimized as an inverse problem based on the above analyses while the spectrum shape is adopted as the objective function. The damage pattern is expressed by the residual strength distribution of the cohesive elements in the estimation scheme. The applied strain is also estimated by the wavelength shift of the reflection spectrum. The damage pattern and the applied strain estimated from the measured spectrum are found to agree with the experimental results.
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U2 - 10.1016/j.compscitech.2005.07.039
DO - 10.1016/j.compscitech.2005.07.039
M3 - Article
AN - SCOPUS:30344451410
SN - 0266-3538
VL - 66
SP - 684
EP - 693
JO - Composites Science and Technology
JF - Composites Science and Technology
IS - 5
ER -