| 000 | 018740000a22003490004500 | ||
|---|---|---|---|
| 003 | EG-GICUC | ||
| 008 | 081226s2006 ua d f m 000 0 eng d | ||
| 040 |
_aEG-GICUC _beng _cEG-GICUC |
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| 041 | 0 | _aeng | |
| 049 | _aDeposite | ||
| 097 | _aM.Sc | ||
| 099 | _aCai01.13.01.M.Sc.2006.Af.R | ||
| 100 | 0 | _aAfifa Adel Shaker Zaki | |
| 245 | 1 | 0 |
_aReliability analysis of the free vibration of composite plates / _cAfifa Adel Shaker Zaki ; Supervised Edward Adeeb Sadek , Mohammad Tawfik Aboelsooud , Wael Gamal Eldeen Abd El rahman |
| 246 | 1 | 5 | _aتحليل الاعتمادية للتذبذب الحر لالواح المواد المركبة |
| 260 |
_aCairo : _bAfifa Adel Shaker Zaki , _c2006 |
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| 300 |
_a127 P. : _bdiagrs ; _c30cm |
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| 502 | _aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering | ||
| 520 | _aThe 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 | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aComposite plates | |
| 653 | 4 | _aForm | |
| 653 | 4 | _aFree vibration | |
| 653 | 4 | _aMPP | |
| 653 | 4 | _aSeem | |
| 700 | 0 |
_aEdward Adeeb Sadek , _eSupervisor |
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| 700 | 0 |
_aMohammad Tawfik Aboelsooud , _eSupervisor |
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| 700 | 0 |
_aWael Gamal Eldeen Abd El rahman , _eSupervisor |
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| 905 |
_aMustafa _eRevisor |
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| 905 |
_aSamia _eCataloger |
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| 942 |
_2ddc _cTH |
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| 999 |
_c34111 _d34111 |
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