TY - JOUR
T1 - On the feasibility of using thermal gradients for active control of interlaminar stresses in laminated composites
AU - Kim, T.
AU - Steadman, D.
AU - Hanagud, S. V.
AU - Atluri, S. N.
N1 - Funding Information:
This work was supported by a grant from the Federal Aviation Administration, to the Center of Excellence for Computational Modeling of Aircraft Structures at Georgia Institute of Technology.
PY - 1997
Y1 - 1997
N2 - In this paper, a method is proposed to actively control interlaminar stresses near the free edges of laminated composites by through-thickness thermal gradients. Theoretical solutions are given for optimal steady-state through-thickness temperature distributions under uniaxial loading that are required to elmininate or reduce the interlaminar stresses below a prescribed level. The optimal solutions are obtained by minimizing appropriate performance indices that are functions of the far-field properties, with respect to the through-thickness temperature differences. In the second part, an experimental investigation is conducted on a glass/epoxy cross-ply laminate with embedded piezoelectric sensors and a thermal heater. Through the experiment, the feasiblity of the thermal control of interlaminar stresses is demonstrated.
AB - In this paper, a method is proposed to actively control interlaminar stresses near the free edges of laminated composites by through-thickness thermal gradients. Theoretical solutions are given for optimal steady-state through-thickness temperature distributions under uniaxial loading that are required to elmininate or reduce the interlaminar stresses below a prescribed level. The optimal solutions are obtained by minimizing appropriate performance indices that are functions of the far-field properties, with respect to the through-thickness temperature differences. In the second part, an experimental investigation is conducted on a glass/epoxy cross-ply laminate with embedded piezoelectric sensors and a thermal heater. Through the experiment, the feasiblity of the thermal control of interlaminar stresses is demonstrated.
UR - http://www.scopus.com/inward/record.url?scp=0030656102&partnerID=8YFLogxK
U2 - 10.1177/002199839703101601
DO - 10.1177/002199839703101601
M3 - Article
AN - SCOPUS:0030656102
SN - 0021-9983
VL - 31
SP - 1556
EP - 1573
JO - Journal of Composite Materials
JF - Journal of Composite Materials
IS - 16
ER -