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Aerodynamic design improvement of wind turbines performance by boundary layer suction / Ayman Mohamed Zaky Hussien ; Supervised Essam E. Khalil Hassan Khalil , Taher Aboudeif , Ahmed Eldegwy

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Ayman Mohamed Zaky Hussien , 2017Description: 115 P. : charts , facsimiles ; 30cmOther title:
  • التصميم الأيروديناميكي لتحسين أداء توربينات الهواء عن طريق شفط الطبقة الجدارية [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering- Department of Mechanical Power Engineering Summary: Egypt has a potential of wind energy exceeds 20,000 MW in the uninhabited desert of the Gulf of Suez area. This research aims to design a wind turbine with rated wind speed matches the average wind speed along the Gulf of Suez area. The design process started with airfoil selection using XFOIL software, then programming a MATLAB code based on the blade- element momentum theory for the 3-D design of the blade and calculation of the net output power. ANSYS Fluent was used for more accurate results. Finally the boundary layer suction concept was implemented for improvement of the blade aerodynamic performance
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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 Cai01.13.11.M.Sc.2017.Ay.A (Browse shelf(Opens below)) Not for loan 01010110072798000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.11.M.Sc.2017.Ay.A (Browse shelf(Opens below)) 72798.CD Not for loan 01020110072798000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering- Department of Mechanical Power Engineering

Egypt has a potential of wind energy exceeds 20,000 MW in the uninhabited desert of the Gulf of Suez area. This research aims to design a wind turbine with rated wind speed matches the average wind speed along the Gulf of Suez area. The design process started with airfoil selection using XFOIL software, then programming a MATLAB code based on the blade- element momentum theory for the 3-D design of the blade and calculation of the net output power. ANSYS Fluent was used for more accurate results. Finally the boundary layer suction concept was implemented for improvement of the blade aerodynamic performance

Issued also as CD

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