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  • 1
    Electronic Resource
    Electronic Resource
    Analysis of laminated composite plates using a higher-order shear deformation theory (1985)
    Chichester [u.a.] : Wiley-Blackwell
    International Journal for Numerical Methods in Engineering 21 (1985), S. 2201-2219 
    Details
    ISSN: 0029-5981
    Keywords: Engineering ; Engineering General
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Mathematics , Technology
    Notes: A higher-order shear deformation theory is used to analyse laminated anisotropic composite plates for deflections, stresses, natural frequencies and buckling loads. The theory accounts for parabolic distribution of the transverse shear stresses, and requires no shear correction coefficients. A displacement finite element model of the theory is developed, and applications of the element to bending, Vibration and stability of laminated plates are discussed. The present solutions are compared with those obtained using the classical plate theory and the three-dimensional elasticity theory.
    Additional Material: 11 Ill.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/nme.1620211207
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    Paper (German National Licenses)
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  • 2
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    Stability and vibration of isotropic, orthotropic and laminated plates according to a higher-order shear deformation theory (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: A higher-order shear deformation theory is used to demonstrate the natural frequencies and buckling loads of elastic plates. The theory accounts for parabolic distribution of the transverse shear strains through the thickness of the plate and rotary inertia. Exact solutions of simply supported plates are obtained and the results are compared with the exact solutions of three-dimensional elasticity theory, the first-order shear deformation theory, and the classical plate theory. The present theory predicts the frequencies and buckling loads more accurately when compared to the first-order and classical plate theories.
    Keywords: STRUCTURAL MECHANICS
    Type: AD-A158472 , Journal of Sound and Vibration (ISSN 0022-460X); 98; 157-170
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Dynamic analysis of laminated plates using a higher-order theory (1984)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: This paper deals with the dynamic analog of the higher-order shear deformation plate theory developed by the senior author. The theory is based on a displacement field in which the inplane displacements are expanded as cubic functions of the thicknes coordinate and the transverse deflection is assumed to be constant through the thickness. The additional dependent unkowns introduced with the quadratic and cubic terms of the thickness coordinate are eliminated by requiring the transverse shear stresses to vanish on the bounding planes of the plate. The theory accounts for the parabolic distribution of the transverse shear stresses, and hence no shear correction coefficients are required.
    Keywords: STRUCTURAL MECHANICS
    Type: AIAA PAPER 84-0977
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Analysis of laminated composite plates using a higher-order shear deformation theory (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-07-12
    Description: A higher-order deformation theory is used to analyse laminated anisotropic composite plates for deflections, stresses, natural frequencies and buckling loads. The theory accounts for parabolic distribution of the transverse shear stresses, and requires no shear correction coefficients. A displacement finite element model of the theory is developed, and applications of the element to bending, vibration and stability of laminated plates are discussed. The present solutions are compared with those obtained using the classical plate theory and the three-dimensional elasticity theory.
    Keywords: STRUCTURAL MECHANICS
    Type: International Journal for Numerical Methods in Engineering (ISSN 0029-5981); 21; 2201-221
    Format: text
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    NASA TECHNICAL REPORTS
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