Aerodynamic characteristics and motion simulation of a damaged aircrafat / Yassir Abbas Awad Elkarim Abdalla ; Supervised Mohammed Madbouli Abdelrahman
Material type: TextLanguage: eng Publication details: Cairo : Yassir Abbas Awad Elkarim Abdalla , 2009Description: 152P. : charts , facsimiles ; 30cmOther title:- الخصائص الايروديناميكية ومحاكاة الحركة لطائرة معطوبة [Added title page title]
- Issued also as CD
Item type | Current library | Home library | Call number | Copy number | Status | Date due | Barcode | |
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Thesis | قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2009.Ya.A (Browse shelf(Opens below)) | Not for loan | 01010110052547000 | |||
CD - Rom | مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2009.Ya.A (Browse shelf(Opens below)) | 52547.CD | Not for loan | 01020110052547000 |
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Cai01.13.01.M.Sc.2009.Mo.N Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme / | Cai01.13.01.M.Sc.2009.Os.A Analysis , design and implementation of a sound tracking system to track and intercept a moving object / | Cai01.13.01.M.Sc.2009.Os.A Analysis , design and implementation of a sound tracking system to track and intercept a moving object / | Cai01.13.01.M.Sc.2009.Ya.A Aerodynamic characteristics and motion simulation of a damaged aircrafat / | Cai01.13.01.M.Sc.2009.Ya.A Aerodynamic characteristics and motion simulation of a damaged aircrafat / | Cai01.13.01.M.Sc.2010.Ah.O Optimization of thrust augmentation ejectors / | Cai01.13.01.M.Sc.2010.Ah.O Optimization of thrust augmentation ejectors / |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
In this thesis panel method is used as a numerical technique . A computer program using Matlab is developed to perform the aerodynamic characteristics and to calculate the aerodynamic coefficients and derivatives as well as the movable control surfaces stability derivatives . The aerodynamics of a damaged aircraft due to the wing fracture horizontal stabilizer fracture aileron fracture elevator fracture and rudder fracture are investigated
Issued also as CD
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