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    Buckling of Laminated Cylindrical Panels Under Uniaxial Compression 

    Source: Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 004:;page 250
    Author(s): K. Chandrashekhara
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Buckling characteristics of anisotropic laminated cylindrical panels are presented using an isoparametric nine-noded rectangular element. Kinematic relations, extended to include the first-order shear ...
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    Analysis of Long Cantilever Cylindrical Shell Subjected to Wind Loading 

    Source: Journal of Engineering Mechanics:;1989:;Volume ( 115 ):;issue: 009
    Author(s): K. Chandrashekhara
    Publisher: American Society of Civil Engineers
    Abstract: Bending analysis of closed cylindrical shells subjected to asymmetric load and having different support conditions is of interest in the design of chimneys, water towers, oil storage tanks, etc. A simple method of analyzing ...
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    Elasticity Solution for a Multilayered Transversely Isotropic Circular Cylindrical Shell 

    Source: Journal of Applied Mechanics:;1982:;volume( 049 ):;issue: 001:;page 108
    Author(s): K. Chandrashekhara; P. Gopalakrishnan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An elasticity solution has been obtained for a long multilayered cylindrical shell of transversely isotropic layers subjected to axisymmetric radial load following Lekhnitskii’s stress function ...
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    Observations on Higher‐Order Beam Theory 

    Source: Journal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 004
    Author(s): A. Bhimaraddi; K. Chandrashekhara
    Publisher: American Society of Civil Engineers
    Abstract: A parabolic shear‐deformation beam theory assuming a higher‐order variation for axial displacement has been recently presented. In this theory, the axial displacement variation can be selected so that it results in a ...
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    Transversely Isotropic Medium with Lined Hole 

    Source: Journal of Engineering Mechanics:;1983:;Volume ( 109 ):;issue: 002
    Author(s): K. Chandrashekhara; P. Gopalakrishnan
    Publisher: American Society of Civil Engineers
    Abstract: An elasticity solution is presented for a semi‐infinite transversely isotropic medium having a circular cylindrical hole with an elastic lining. The lining is analyzed as an orthotropic shell. The general solution obtained ...
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    Deflections and Stresses of Antisymmetric Angle-Ply Clamped Plates Under Transverse Loading 

    Source: Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 003:;page 210
    Author(s): A. H. Yahyavi; K. Chandrashekhara
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Closed-form solutions are not tractable for clamped composite plates due to the boundary conditions and anisotropy of the plate. In the present work, a method based on Lagrange multipliers is ...
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    Photoelastic Analysis of a Composite Prism Subjected to Partial Compression 

    Source: Journal of Applied Mechanics:;1978:;volume( 045 ):;issue: 002:;page 436
    Author(s): K. A. Jacob; K. Chandrashekhara
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Static Analysis of Thick Laminated Circular Cylindrical Shells 

    Source: Journal of Pressure Vessel Technology:;1993:;volume( 115 ):;issue: 002:;page 193
    Author(s): K. Chandrashekhara; B. S. Kumar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate solution for a thick laminated simply supported circular cylindrical shell of revolution and shell panel subjected to asymmetric load has been obtained using elasticity approach. ...
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    Static Analysis of Infinite Laminated Cylindrical Shell Panel 

    Source: Journal of Aerospace Engineering:;1998:;Volume ( 011 ):;issue: 001
    Author(s): K. Chandrashekhara; K. S. Nanjunda Rao
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents an approximate three-dimensional elasticity solution for an infinitely long, cross-ply laminated circular cylindrical shell panel with simply supported boundary conditions, subjected to an arbitrary ...
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    Analysis of a Long Thick Orthotropic Circular Cylindrical Shell Panel 

    Source: Journal of Engineering Mechanics:;1996:;Volume ( 122 ):;issue: 006
    Author(s): K. Chandrashekhara; K. S. Nanjunda Rao
    Publisher: American Society of Civil Engineers
    Abstract: An exact three-dimensional elasticity solution has been obtained for an infinitely long, thick transversely isotropic circular cylindrical shell panel, simply supported along the longitudinal edges and subjected to a radial ...
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