Variable fidelity design optimization of subsonic aircraft air intake /
Mohamed Hassan Ali
Variable fidelity design optimization of subsonic aircraft air intake / دراسة متعددة الثقة للحصول على أفضل تصميم لمدخل الهواء للطائرات Mohamed Hassan Ali ; Supervised Mohamed Madbouli Abdelrahman - Cairo : Mohamed Hassan Ali , 2008 - 113P. : charts , facsimiles ; 30cm
Thesis(M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
The aircraft air intake is one of the most important parts in the layout design of modern fighter and trainer aircraft most of the aircrafts famous for their good maneuvers have a well designed air intake which is capable of tolerating high angles of attack and large sideslip angles without significant pressure losses and the engine thrust in return
Finite element Flutter Piezoelectric
Variable fidelity design optimization of subsonic aircraft air intake / دراسة متعددة الثقة للحصول على أفضل تصميم لمدخل الهواء للطائرات Mohamed Hassan Ali ; Supervised Mohamed Madbouli Abdelrahman - Cairo : Mohamed Hassan Ali , 2008 - 113P. : charts , facsimiles ; 30cm
Thesis(M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
The aircraft air intake is one of the most important parts in the layout design of modern fighter and trainer aircraft most of the aircrafts famous for their good maneuvers have a well designed air intake which is capable of tolerating high angles of attack and large sideslip angles without significant pressure losses and the engine thrust in return
Finite element Flutter Piezoelectric