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  • 1
    Electronic Resource
    Electronic Resource
    Amsterdam : Elsevier
    International Journal of Non-Linear Mechanics 23 (1988), S. 217-229 
    ISSN: 0020-7462
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Amsterdam : Elsevier
    International Journal of Non-Linear Mechanics 25 (1990), S. 263-273 
    ISSN: 0020-7462
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Amsterdam : Elsevier
    Journal of Sound and Vibration 167 (1993), S. 129-147 
    ISSN: 0022-460X
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Type of Medium: Electronic Resource
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  • 4
    Electronic Resource
    Electronic Resource
    Springer
    Mechanics of composite materials 6 (1970), S. 174-175 
    ISSN: 1573-8922
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Type of Medium: Electronic Resource
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  • 5
    Electronic Resource
    Electronic Resource
    Springer
    International journal of fracture 57 (1992), S. 151-166 
    ISSN: 1573-2673
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The analytical determination of the time history of stress intensity factors near a through crack in an impacted symmetrically cross-ply laminated composite plate constitutes the main objective of this investigation. Toward the end of removing the shortcomings implied by the use of the classical plate theory when dealing with crack problems, herein the theory of composite plates based upon discarding Kirchhoff hypothesis is employed. It incorporates the effects of transverse shear deformations, transverse normal stress and rotatory inertias and fulfills the tangential conditions on the bounding planes of the plate. As a result, this theory permits the prescription of three boundary conditions on each edge, a fact which renders it very adequate for the problem studied herein. The plate is considered impacted by a bending moment, applied to the surface of the finite crack. By the use of the integral transform technique the problem is reduced to solving a pair of dual integral equations and, further, to the solution of a Fredholm integral equation of the second kind. The numerical illustrations emphasize the effects played by transverse shear deformations and geometric and material properties of the laminate on stress intensity factor history.
    Type of Medium: Electronic Resource
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  • 6
    Electronic Resource
    Electronic Resource
    Springer
    Journal of engineering mathematics 28 (1994), S. 407-425 
    ISSN: 1573-2703
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mathematics , Technology
    Notes: Abstract A simple refined discrete-layer theory of anisotropic laminated composite plates is substantiated. The theory is based on the assumption of a piecewise linear variation of the in-plane displacement components and of the constancy of the transverse displacement throughout the thickness of the laminate. This plate model incorporates transverse shear deformation, dynamic and thermal effects as well as the geometrical non-linearities and fulfills the continuity conditions for the displacement components and transverse shear stresses at the interfaces between laminae. As it is shown in the paper, the refinement implying the fulfillment of continuity conditions is not accompanied by an increase of the number of independent unknown functions, as implied in the standard first order transverse shear deformation theory. It is also shown that the within the framework of the linearized static counterpart of the theory, several theorems analogous to the ones in the 3-D elasticity theory could be established. These concern the energetic theorems, Betti's reciprocity theorem, the uniqueness theorem for the solutions of boundary-value problems of elastic composite plates, etc. Finally, comparative remarks on the present and standard first order transverse shear deformation theories are made and pertinent conclusions about its usefulness and further developments are outlined.
    Type of Medium: Electronic Resource
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  • 7
    Electronic Resource
    Electronic Resource
    Springer
    International journal of fracture 96 (1999), S. 17-35 
    ISSN: 1573-2673
    Keywords: Interfacial damage ; displacement jump ; load-carrying capacity ; buckling strength ; zig-zag nonlinear plate model.
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The problem of the implications of interfacial damage on the local and global static response of cross-ply laminated flat structures is addressed in this paper. As a basic prerequisite, a third-order generalized zig-zag nonlinear plate theory incorporating the effect of interfacial damage is used. The theory rests upon a representation of the displacement field which: (i) fulfills a priori the shear traction continuity conditions at each interface of the laminate and the free shear traction conditions on the top and bottom external planes of the plate, (ii) satisfies the requirement of continuous displacements at the perfectly bonded interfaces, and (iii) incorporates the interfacial tangential displacement jump condition when slip-type interlayer imperfections are present. The theory also incorporates the geometrical nonlinearities and the thermal effects. Numerical results highlighting the effect of interfacial damage on the static response of laminated composite plates in cylindrical bending are displayed and conclusions on their implications upon their load-carrying capacity are outlined.
    Type of Medium: Electronic Resource
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  • 8
    ISSN: 1619-6937
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Type of Medium: Electronic Resource
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  • 9
    ISSN: 1619-6937
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Summary This paper establishes, on a quantitative basis, the correlation between two apparently different higher-order theories of anisotropic plates. In addition it provides a strong mathematical tool allowing one to determine, in an exact and unified manner, the state of stress of orthotropic shear deformable rectangular plates exhibiting a variety of edge conditions.
    Type of Medium: Electronic Resource
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  • 10
    Electronic Resource
    Electronic Resource
    Springer
    Acta mechanica 96 (1993), S. 203-224 
    ISSN: 1619-6937
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Summary The vibrational behavior of geometrically imperfect single and multilayered composite double-curved shallow panels subjected to a system of tangential compressive/tensile edge loads in the pre- and postbuckling ranges is investigated. The effects of transverse shear deformations, lamination, the character of in-plane boundary conditions, and of transverse normal stress are incorporated and their influence is emphasized. Numerical illustrations enabling one to compare the obtained results based on higher order and first order shell theories with their classical counterparts, based on the Love-Kirchhoff model are presented and conclusions related to their range of applicability are outlined.
    Type of Medium: Electronic Resource
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