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العنوان
Improvement of aerodynamic performance of aircraft wing /
الناشر
Hesham Shahat Mohamed Helal ,
المؤلف
Hesham Shahat Mohamed Helal
هيئة الاعداد
باحث / Hesham Shahat Mohamed Helal
مشرف / Essam E. Khalil Hassan
مشرف / Osama Ezzat Abdellatif
مشرف / Gamal Abdelmonim Elhariry
تاريخ النشر
2016
عدد الصفحات
157 P. :
اللغة
الإنجليزية
الدرجة
الدكتوراه
التخصص
الهندسة الميكانيكية
تاريخ الإجازة
9/3/2016
مكان الإجازة
جامعة القاهرة - كلية الهندسة - MECHANICAL POWER ENGINEERING
الفهرس
Only 14 pages are availabe for public view

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from 192

Abstract

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 ®