Improvement of aerodynamic performance of aircraft wing / Hesham Shahat Mohamed Helal ; Supervised Essam E. Khalil Hassan , Osama Ezzat Abdellatif , Gamal Abdelmonim Elhariry

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Hesham Shahat Mohamed Helal

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Material type: Text

TextLanguage: English Publication details: Cairo : Hesham Shahat Mohamed Helal , 2016Description: 157 P. : facsimiles ; 30cmOther title:

تحسين أداء الديناميكا الهوائية لجناح الطائرة [Added title page title]

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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering Summary: Aircraft designers are performing research to improve the overall aircraft efficiency which would be useful both for aircraft manufacturer and airlines. A winglet is a system used to enhance the effectiveness of air plane by increasing lift {u2013}to- drag ratio (L/D).The target of this investigation is compare the aerodynamic characteristics of the wing with and without winglet. For the this study, thesis considered raked winglet with four angles and considered the optimum angle to study the effect of taper ratios and then study blended winglet at four angles, and considered the optimum angle to study the effect of taper ratios, study the effect of length of winglet and Mach number ,using CFD simulation performs by FLUENT ®

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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.2016.He.I (Browse shelf(Opens below))		Not for loan		01010110070878000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.11.Ph.D.2016.He.I (Browse shelf(Opens below))	70878.CD	Not for loan		01020110070878000

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

Aircraft designers are performing research to improve the overall aircraft efficiency which would be useful both for aircraft manufacturer and airlines. A winglet is a system used to enhance the effectiveness of air plane by increasing lift {u2013}to- drag ratio (L/D).The target of this investigation is compare the aerodynamic characteristics of the wing with and without winglet. For the this study, thesis considered raked winglet with four angles and considered the optimum angle to study the effect of taper ratios and then study blended winglet at four angles, and considered the optimum angle to study the effect of taper ratios, study the effect of length of winglet and Mach number ,using CFD simulation performs by FLUENT ®

Issued also as CD

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