header
Local cover image
Local cover image
Image from OpenLibrary

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

By: Contributor(s): Material type: TextTextLanguage: 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]
Subject(s): Online resources: Available additional physical forms:
  • Issued also as CD
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
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Home library Call number Copy number Status Barcode
Thesis 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 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

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

There are no comments on this title.

to post a comment.

Click on an image to view it in the image viewer

Local cover image