Mohamed Ahmed Mohamed Hussein Aziz  <br/><br/>
Design optimization of a three dimensional supersonic intake /  
 الحصول على التصميم الأمثل لمدخل الهواء للطائرات فائقة السرعة 
Mohamed Ahmed Mohamed Hussein Aziz ; Supervised Mohamed Madbouli Abdelrahman , Hesham Mahmoud Elbanna 
 - Cairo :   Mohamed Ahmed Mohamed Hussein Aziz ,   2010 
 - 203P. :   charts , facsimiles ;   30cm 
<br/><br/>Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering 
<br/><br/> 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 
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<br/><br/><label>Subjects--Index Terms: </label>Air intake  Optimum design  Supersonic aircraft