TY  - BOOK
AU  - Mohamed Ahmed Mohamed Hussein Aziz 
AU  - Hesham Mahmoud Elbanna , 
AU  - Mohamed Madbouli Abdelrahman , 
TI  - Design optimization of a three dimensional supersonic intake / 
PY  - 2010///
CY  - Cairo : 
PB  - Mohamed Ahmed Mohamed Hussein Aziz , 
KW  - Air intake
KW  - Optimum design
KW  - Supersonic aircraft
N1  - Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering; Issued also as CD
N2  - 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
ER  -