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contributor authorChaubey Abhay Kumar;Kumar Ajay;Mishra S. S.
date accessioned2019-02-26T07:34:33Z
date available2019-02-26T07:34:33Z
date issued2018
identifier other%28ASCE%29AS.1943-5525.0000881.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4248011
description abstractThe present paper is the first study of free vibration analysis of laminated composite rhombic (skew) elliptic paraboloids with mass variation via multiple cutouts and concentrated mass. To solve the vibration problem of a laminated composite skew elliptic paraboloid with multiple cutouts and concentrated mass, cubic variation in the displacement field and cross-curvature effects of the shell are considered. The parabolic variation of transverse shear strain is considered; hence, no shear correction factor is required. The zero transverse shear stress conditions at the top and bottom of the shell are imposed in the mathematical model. The finite-element implementation of the present realistic mathematical model is done using a nine-noded curved isoparametric element with seven unknowns at each node. The C finite-element (FE) implementation of the present mathematical model has been done and coded in FORTRAN. The present model results are compared and found in good agreement with experimental, analytical, and other solutions published in the literature. A free vibration study has been done for skew elliptic paraboloids with multiple cutouts and concentrated mass having different curvatures, ply orientations, and thickness ratios.
publisherAmerican Society of Civil Engineers
titleDynamic Analysis of Laminated Composite Rhombic Elliptic Paraboloid due to Mass Variation
typeJournal Paper
journal volume31
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000881
page4018059
treeJournal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 005
contenttypeFulltext


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