Variable fidelity design optimization of subsonic aircraft air intake / Mohamed Hassan Ali ; Supervised Mohamed Madbouli Abdelrahman
Language: Eng Publication details: Cairo : Mohamed Hassan Ali , 2008Description: 113P. : charts , facsimiles ; 30cmOther title:- دراسة متعددة الثقة للحصول على أفضل تصميم لمدخل الهواء للطائرات [Added title page title]
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قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2008.Mo.V (Browse shelf(Opens below)) | Not for loan | 01010110050293000 | ||
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مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2008.Mo.V (Browse shelf(Opens below)) | 50293.CD | Not for loan | 01020110050293000 |
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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
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