Experimental and numerical investigation of the effects of winglets on aircraft wings / Mohamed Ahmed Ibrahim Mohamed Khalifa ; Supervised Abdelmotaleb Ali Mostafa , Osama Ezzat Abdellatif

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Mohamed Ahmed Ibrahim Mohamed Khalifa

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TextLanguage: English Publication details: Cairo : Mohamed Ahmed Ibrahim Mohamed Khalifa , 2017Description: 141 P. : charts , facsimiles ; 30cmOther title:

دراسة عملية ونظرية عن تأثيرات الجنيحات على أجنحة الطـائرات [Added title page title]

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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering Summary: Experimental and numerical investigation of the effects of winglets on an aircraft wing performance and structure is presented. A 3-D winglets analysis is performed on a civil aircraft wing. The study was divided into three stages. In the first stage, three wings using CFD software are numerically investigated. In the second stage, the aerodynamic characteristic around a civil aircraft wing are measured, and in the final stage, structure analysis using FEM is performed. The numerical results are in good agreement with experimental data and show blended connection enhances the lift coefficient appreciably. The structure results show composite material reduces wing weight

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Item type	Current library	Home library	Call number	Copy number	Status	Date due	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.11.Ph.D.2017.Mo.E (Browse shelf(Opens below))		Not for loan		01010110074287000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.11.Ph.D.2017.Mo.E (Browse shelf(Opens below))	74287.CD	Not for loan		01020110074287000

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

Experimental and numerical investigation of the effects of winglets on an aircraft wing performance and structure is presented. A 3-D winglets analysis is performed on a civil aircraft wing. The study was divided into three stages. In the first stage, three wings using CFD software are numerically investigated. In the second stage, the aerodynamic characteristic around a civil aircraft wing are measured, and in the final stage, structure analysis using FEM is performed. The numerical results are in good agreement with experimental data and show blended connection enhances the lift coefficient appreciably. The structure results show composite material reduces wing weight

Issued also as CD

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