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OverviewAnalytical solution using Ritz method and Fourier series is used to determine thermal buckling of laminated composite thin plates at a general elastic boundary condition applied to in-plane uniform temperature distribution, also the natural frequencies under an initial thermal load of laminated composite thin plates are investigated depending upon Classical laminated plate theory (CLPT). A generalized procedure solution is developed for the Rayleigh-Ritz method combined with the imaginary spring technique. Employing the principle of virtual work the equation of motion of the plates was derived, and by employing a modified Fourier displacement function was solved, that satisfies general edge conditions. The transverse deflection and rotation due to bending o the plate are developed into principle Fourier series with a sufficient smoothness auxiliary polynomial function, the variable of boundary condition can be easily done by only change the boundary spring stiffness of the all boundaries of the laminated composite plate without achieving any replacement to the solution. Full Product DetailsAuthor: Mohammed Alabas , Widad Ibraheem MajeedPublisher: Noor Publishing Imprint: Noor Publishing Dimensions: Width: 15.20cm , Height: 0.80cm , Length: 22.90cm Weight: 0.209kg ISBN: 9786200075215ISBN 10: 6200075212 Pages: 136 Publication Date: 20 January 2020 Audience: General/trade , General Format: Paperback Publisher's Status: Active Availability: In stock We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |