TY - GEN
T1 - Health and usage monitoring of aging helicopter structure using fiber Bragg grating sensor net
AU - Kressel, I.
AU - Balter, J.
AU - Evenhaim, S.
AU - Leibovich, H.
AU - Gruskeiwicz, D.
AU - Glam, B.
AU - Shemesh, N. N.Y.
AU - Kedem, S.
AU - Elbaz, D.
AU - Gali, S.
AU - Tur, M.
PY - 2011
Y1 - 2011
N2 - Sensing the high strains area in the patch over the crack is the goal of the proposed SHM concept. It is clearly seen that the thermally induced strain in the patch, over the crack area, changes significantly. It is concluded that a sensor net with a low spatial resolution should be sufficient to detect the existence of a critical crack.
AB - Sensing the high strains area in the patch over the crack is the goal of the proposed SHM concept. It is clearly seen that the thermally induced strain in the patch, over the crack area, changes significantly. It is concluded that a sensor net with a low spatial resolution should be sufficient to detect the existence of a critical crack.
UR - http://www.scopus.com/inward/record.url?scp=84866886311&partnerID=8YFLogxK
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AN - SCOPUS:84866886311
SN - 9781617824012
T3 - 51st Israel Annual Conference on Aerospace Sciences 2011
SP - 144
EP - 145
BT - 51st Israel Annual Conference on Aerospace Sciences 2011
T2 - 51st Israel Annual Conference on Aerospace Sciences 2011
Y2 - 23 February 2011 through 24 February 2011
ER -