Thermal Response of Symmetric Cross-Ply Laminated Plates Subjected to Linear and Non-Linear Thermo-Mechanical Loads

Ghugal, Yuwaraj M.; Kulkarni, S. K.

doi:10.1080/01495739.2013.770664

Cited by 10 publications

(2 citation statements)

References 22 publications

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“…Mechab et al [43] developed a new trigonometric shear deformation theory for the thermo-mechanical analysis of laminated composite plates. Ghugal and Kulkarni [44][45][46][47] have applied trigonometric shear deformation theory (TSDT) for the thermal analysis of cross-ply laminated plates. A higherorder shear deformation theory with Taylor series-type expansion in the thickness direction for the displacements has been developed by Kant and Khare [48] for composite and sandwich plates under thermal loading.…”

Section: Introductionmentioning

confidence: 99%

A Four-Variable Plate Theory for Thermoelastic Bending Analysis of Laminated Composite Plates

Sayyad

Ghugal²,

Mhaske

2015

Journal of Thermal Stresses

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In this article, the thermoelastic bending analysis of laminated composite plates subjected to thermal load linear across the thickness using the four variable refined plate theory is presented. The theory involves four unknown variables, as against five in case of other higher-order theories and first-order shear deformation theory. The theory gives rise to transverse shear stress variation such that the transverse shear stresses vary parabolically across the thickness satisfying shear stress free conditions at top and bottom surfaces of the plate. The theory does not require problem-dependent shear correction factors that are associated with the first-order shear deformation theory. The principle of virtual work is used to obtain variationally consistent governing equations and boundary conditions. The simply supported laminated composite plates are considered for the detail numerical study. A closed-form solution is obtained using the double trigonometric series technique suggested by Navier. The numerical results for thermal displacements and stresses of laminated composite plates are obtained and compared with those of other refined theories and exact solutions wherever applicable to assess the efficiency of the present theory. From the numerical results it is observed that since plate is subjected to pure thermal load and not subjected to transverse mechanical load, the present theory has strong similarity with classical plate theory in many aspects.

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Section: Introductionmentioning

confidence: 99%

A Four-Variable Plate Theory for Thermoelastic Bending Analysis of Laminated Composite Plates

Sayyad

Ghugal²,

Mhaske

2015

Journal of Thermal Stresses

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“…The results showed the effects of geometry, material and lamination parameters of woven fiber laminate on the vibration of composite plates for different temperature. Ghugal [17] presented the flexural response of cross-ply laminated plates subjected to thermo-mechanical loads. The shear deformation theory satisfies the shear stress free boundary conditions on the top and bottom surfaces of the plate.…”

Section: Introductionmentioning

confidence: 99%

Thermally induced stability and vibration of initially stressed laminated composite plates

Chen¹,

Chen

Lin³

2016

mech

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Effect of Degree of Orthotropy on Transverse Deflection of Composite Laminates Under Thermal Load

Kulkarni¹,

Ghugal²

2014

Advances in Structural Engineering

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Thermal Response of Symmetric Cross-Ply Laminated Plates Subjected to Linear and Non-Linear Thermo-Mechanical Loads

Cited by 10 publications

References 22 publications

A Four-Variable Plate Theory for Thermoelastic Bending Analysis of Laminated Composite Plates

A Four-Variable Plate Theory for Thermoelastic Bending Analysis of Laminated Composite Plates

Thermally induced stability and vibration of initially stressed laminated composite plates

Effect of Degree of Orthotropy on Transverse Deflection of Composite Laminates Under Thermal Load

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