Design optimization of a three dimensional supersonic intake /
Mohamed Ahmed Mohamed Hussein Aziz
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
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
Air intake Optimum design Supersonic aircraft
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
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
Air intake Optimum design Supersonic aircraft