The Effect of Shape Memory Alloy Embeddings on the Nonlinear Flutter of Composite Panels Subject To Thermal and Random Acoustic Loads / Hesham Hamed Ahmed Ibrahim ; Supervised Hani Mohammed Negmy , Mohammed Nader Abuelfoutouh , Mohammad Tawfik Aboelsooud
Language: Eng Publication details: Cairo : Hesham Hamed Ahmed Ibrahim , 2007Description: 148P. : ill. ; 30CmOther title:- تأثيرمطعمات السبائك الذاكرة للشكل على الرفرفة غير الخطية للألواح المركبة المعرضة لأحمال حرارية وصوتية عشوائية [Added title page title]
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قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.Ph.D.2007.He.E (Browse shelf(Opens below)) | Not for loan | 01010110047065000 | ||
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مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.Ph.D.2007.He.E (Browse shelf(Opens below)) | 47065.CD | Not for loan | 01020110047065000 |
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| Cai01.13.01.Ph.D.2006.Mo.F. Fault diagnosis for hydrualic system using neural network / | Cai01.13.01.Ph.D.2007.Am.D Design optimization of centrifugal compressor impeller / | Cai01.13.01.Ph.D.2007.Am.D Design optimization of centrifugal compressor impeller / | Cai01.13.01.Ph.D.2007.He.E The Effect of Shape Memory Alloy Embeddings on the Nonlinear Flutter of Composite Panels Subject To Thermal and Random Acoustic Loads / | Cai01.13.01.Ph.D.2007.He.E The Effect of Shape Memory Alloy Embeddings on the Nonlinear Flutter of Composite Panels Subject To Thermal and Random Acoustic Loads / | Cai01.13.01.Ph.D.2007.Mo.P Predication of strucctural damage under impact loads / | Cai01.13.01.Ph.D.2007.Mo.P Predication of strucctural damage under impact loads / |
Thesis (Ph.D.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering
In this work , a traditional composite plate impregnated with pre - strained shape memory alloy (SMA) fibers and subject to the combined effect of thermal , aerodynamic , and acoustic loads , is investigated to demonstrate the effectiveness of using the SMA fiber embeddings in improving the static and dynamic response of composite plates.A new nonlinear finite element model is presented using the first - order shear plate theory and von Karman strain displacement relations , assuming thermal strain being a cumulative quantity.The governing equations are obtained using the principle of virtual work.
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