Aerodynamic characteristics and motion simulation of a damaged aircrafat /
Yassir Abbas Awad Elkarim Abdalla
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
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
Aerodynamic derivatives Panel method Potential flow
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
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
Aerodynamic derivatives Panel method Potential flow