A higher order displacement model based on a cubic axial strain, cubic transverse shear strain and quadratic transverse normal strain across the thickness of the beam, to model exactly the warping of the cross section is proposed which maintains zero stress at the top and bottom of the beam with out the aid of any shear correction factor. Numerical experiments carried out clearly bring out the efficacy of this model over the first order theory for laminated beams.

1.
Kant
T.
, and
Gupta
A.
,
1988
, “
A Finite Element Model for a Higher-Order Shear-Deformable Beam Theory
,”
Journal of Sound and Vibration
, Vol.
125
, pp.
193
202
.
2.
Kant
T.
,
Marur
S. R.
, and
Rao
G. S.
, “
Analytical Solution to the Dynamic Analysis of Laminated Beams Using Higher Order Refined Theory
,”
Journal of Composite Structures
, Vol.
40
, pp.
1
10
.
3.
Marur
S. R.
, and
Kant
T.
,
1996
, “
Free Vibration Analysis of Fiber Reinforced Composite Beams Using Higher Order Theories and Finite Element Modelling
,”
Journal of Sound and Vibration
, Vol.
194
, pp.
337
351
.
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