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Finite element formulation of nonlinear flutter of laminated composite panels under thermal and yawed flow effects with active suppression / Mohamed Lotfy Taha Hassan ; Supervised Sayed Desouki Hassan , Mohamed Madbouly Abdelrahman , Mokhtar Malek Elnomrossy

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Mohamed Lotfy Taha Hassan , 2012Description: 152 P. : charts , facsimiles ; 30cmOther title:
  • صياغة ودراسة تاثير الحرارة والسريان المائل والتحكم الفعال على الرفرفة اللاخطية للألواح المصنوعة من المواد المركبة باستخدام طريقة العناصر المحدودة [Added title page title]
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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: A finite element model is formulated for investigating aero- thermo- elastic behaviour of laminated composite and isotropic panels subject to yawed flow and elevated temperatures . The first - order quasi - steady piston theory is employed for evaluating the aerodynamic pressure. The quasi- steady thermal stress theory is used for representing thermal stresses
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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.Ph.D.2012.Mo.F (Browse shelf(Opens below)) Not for loan 01010110059963000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.Ph.D.2012.Mo.F (Browse shelf(Opens below)) 59963.CD Not for loan 01020110059963000

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

A finite element model is formulated for investigating aero- thermo- elastic behaviour of laminated composite and isotropic panels subject to yawed flow and elevated temperatures . The first - order quasi - steady piston theory is employed for evaluating the aerodynamic pressure. The quasi- steady thermal stress theory is used for representing thermal stresses

Issued also as CD

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