Elastic and aeroelastic analysis of aircraft metallic, composite, and smart wings / Mohamed Abdou Mahran Kasem ; Supervised Hani M. Negm , Adel M. Elsabbagh

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Mohamed Abdou Mahran Kasem

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TextLanguage: English Publication details: Cairo : Mohamed Abdou Mahran Kasem , 2018Description: 103 P. : charts , facsimiles , photographs ; 30cmOther title:

تحليل المرونه و المرونه الهوائيه للأجنحة المعدنية و المركبة ذات التراجع مع وجود مواد ذكيه كهربيه اجهادية [Added title page title]

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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: In the present dissertation elastic and aeroelastic models are developed for the analysis of metallic and composite wings with attached piezoelectric actuators using the finite element method. The elastic and aeroelastic problems were modeled as eigenvalue problems. The piezoelectric potential effect is integrated as prestresses using the concept of geometric stiffness. The analysis covers 2-D and 3-D wings, and the effect of engine mass

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Item type	Current library	Home library	Call number	Copy number	Status	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.01.Ph.D.2018.Mo.E (Browse shelf(Opens below))		Not for loan	01010110077263000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.01.Ph.D.2018.Mo.E (Browse shelf(Opens below))	77263.CD	Not for loan	01020110077263000

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Previous	Cai01.13.01.Ph.D.2018.Ho.I Improving dynamic and aeroelastic performance of helicopter rotors using periodic design and piezo active control /	Cai01.13.01.Ph.D.2018.Ho.I Improving dynamic and aeroelastic performance of helicopter rotors using periodic design and piezo active control /	Cai01.13.01.Ph.D.2018.Mo.E Elastic and aeroelastic analysis of aircraft metallic, composite, and smart wings /	Cai01.13.01.Ph.D.2018.Mo.E Elastic and aeroelastic analysis of aircraft metallic, composite, and smart wings /	Cai01.13.01.Ph.D.2019.Am.E Experimental and numerical investigation of the effect of vertical axis wind turbine blade cascading on the dynamic stall phenomenon /	Cai01.13.01.Ph.D.2019.Am.E Experimental and numerical investigation of the effect of vertical axis wind turbine blade cascading on the dynamic stall phenomenon /	Cai01.13.01.Ph.D.2019.Mo.D Design and implementation of rate table framework for autopilot testing /	Next

Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

In the present dissertation elastic and aeroelastic models are developed for the analysis of metallic and composite wings with attached piezoelectric actuators using the finite element method. The elastic and aeroelastic problems were modeled as eigenvalue problems. The piezoelectric potential effect is integrated as prestresses using the concept of geometric stiffness. The analysis covers 2-D and 3-D wings, and the effect of engine mass

Issued also as CD

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