Yassir Abbas Awad Elkarim Abdalla <br/><br/>
Aerodynamic characteristics and motion simulation of a damaged aircrafat /  
 الخصائص الايروديناميكية ومحاكاة الحركة لطائرة معطوبة 
Yassir Abbas Awad Elkarim Abdalla ; Supervised Mohammed Madbouli Abdelrahman 
 - Cairo :   Yassir Abbas Awad Elkarim Abdalla ,   2009 
 - 152P. :   charts , facsimiles ;   30cm 
<br/><br/>Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering 
<br/><br/> 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 
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<br/><br/><label>Subjects--Index Terms: </label>Aerodynamic derivatives Panel method  Potential flow