Design optimization of a three dimensional supersonic intake / Mohamed Ahmed Mohamed Hussein Aziz ; Supervised Mohamed Madbouli Abdelrahman , Hesham Mahmoud Elbanna
Material type: TextLanguage: eng Publication details: Cairo : Mohamed Ahmed Mohamed Hussein Aziz , 2010Description: 203P. : charts , facsimiles ; 30cmOther title:- الحصول على التصميم الأمثل لمدخل الهواء للطائرات فائقة السرعة [Added title page title]
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Item type | Current library | Home library | Call number | Copy number | Status | Date due | Barcode | |
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Thesis | قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2010.Mo.D (Browse shelf(Opens below)) | Not for loan | 01010110053374000 | |||
CD - Rom | مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2010.Mo.D (Browse shelf(Opens below)) | 53374.CD | Not for loan | 01020110053374000 |
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Cai01.13.01.M.Sc.2010.Ah.O Optimization of thrust augmentation ejectors / | Cai01.13.01.M.Sc.2010.Ah.O Optimization of thrust augmentation ejectors / | Cai01.13.01.M.Sc.2010.Mo.D Design optimization of a three dimensional supersonic intake / | Cai01.13.01.M.Sc.2010.Mo.D Design optimization of a three dimensional supersonic intake / | Cai01.13.01.M.Sc.2010.Pe.F Finite element and experimental models of an adaptive magnetorheological sandwich beam structure / | Cai01.13.01.M.Sc.2010.Pe.F Finite element and experimental models of an adaptive magnetorheological sandwich beam structure / | Cai01.13.01.M.Sc.2011.Ah.E Efficient domain decomposition technique for solution of wave scattering in non-uniform flows / |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
In this thesis a computer program using Matlab and Python are developed to perform an optimization cycle to design an air intake for supersonic aircraft . First a preliminarily design step this is carried out by calculating Mach number air angles and pressures distributions along the intake . Second a high fidelity design optimization step by using the result of step one and computational fluid dynamics programs (CFD - RC package ) and utilize the simplex algorithm inside the package to obtain the optimun design
Issued also as CD
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