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    Analysis of Hybrid Laminated Composite Plates 

    Source: Journal of Aerospace Engineering:;1990:;Volume ( 003 ):;issue: 001
    Author(s): S. P. Joshi; N. G. R. Iyengar
    Publisher: American Society of Civil Engineers
    Abstract: Hybrid laminated composite plates are analyzed using a nine‐noded isoparametric plate finite element based on Mindlin's theory. The shear flexibility is included in the finite element modeling. Shear flexibility is of ...
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    Programming Methods in Structural Dynamics 

    Source: Journal of Vibration and Acoustics:;1983:;volume( 105 ):;issue: 004:;page 411
    Author(s): N. G. R. Iyengar; H. Saunders; S. K. Gupta
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Stress Relaxation in the Sn-Pb Eutectic Alloy 

    Source: Journal of Engineering Materials and Technology:;1975:;volume( 097 ):;issue: 002:;page 187
    Author(s): G. S. Murty; U. P. Singh; N. G. R. Iyengar
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Stability of Curved Composite Panels with Random Material Properties 

    Source: Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002
    Author(s): Bhrigu N. Singh; N. G. R. Iyengar; Dayanand Yadav
    Publisher: American Society of Civil Engineers
    Abstract: The initial buckling behavior of thick laminated composite curved panels with random material properties subjected to various in-plane edge loads has been investigated. For this purpose, an approach is presented to obtain ...
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    Effects of Random Material Properties on Buckling of Composite Plates 

    Source: Journal of Engineering Mechanics:;2001:;Volume ( 127 ):;issue: 009
    Author(s): Bhrigu N. Singh; N. G. R. Iyengar; Dayanand Yadav
    Publisher: American Society of Civil Engineers
    Abstract: Composites exhibit a considerable amount of variation in their material properties because their fabrication/manufacturing process involves a large number of parameters that cannot be controlled effectively. In the present ...
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