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Reliability analysis of the free vibration of composite plates / Afifa Adel Shaker Zaki ; Supervised Edward Adeeb Sadek , Mohammad Tawfik Aboelsooud , Wael Gamal Eldeen Abd El rahman

By: Contributor(s): Language: English Publication details: Cairo : Afifa Adel Shaker Zaki , 2006Description: 127 P. : diagrs ; 30cmOther title:
  • تحليل الاعتمادية للتذبذب الحر لالواح المواد المركبة [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: The aim of this work is to perform reliability analysis of the free vibration of a composite plate with material and fabrication uncertainties using the Stochastic Finite Element MethodThe stochastic analysis is performed using the First Order Reliability Method (FORM - method 2) and the Second Order Reliability Method (SORM) In order to apply either of these techniques , a set of random variables is initially selectedThe basic random variables include laminae stiffness properties and material density , as well as the randomness in ply orientation angles which results from fabrication
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2006.Af.R (Browse shelf(Opens below)) Not for loan 01010110045871000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2006.Af.R (Browse shelf(Opens below)) 45871.CD Not for loan 01020110045871000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

The aim of this work is to perform reliability analysis of the free vibration of a composite plate with material and fabrication uncertainties using the Stochastic Finite Element MethodThe stochastic analysis is performed using the First Order Reliability Method (FORM - method 2) and the Second Order Reliability Method (SORM) In order to apply either of these techniques , a set of random variables is initially selectedThe basic random variables include laminae stiffness properties and material density , as well as the randomness in ply orientation angles which results from fabrication

Issued also as CD

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