| This thesis presents the empirical method to calculate the aerodynamic coefficients on the deformable wing.Besides some empirical method,the small disturbing theory?taper flow theory?lifting surface theory were applied in this paper.By these theory and empirical method,this paper arrives a suit of method to calculate the aerodynamic characteristics of the deformable wing.Bases this calculations, author has developed the computation program himselfln addition,the program was appled to discuss the aerodynamic coefficients in different ving aspect ratio and wing sweep angle cases,the effect of Mach number,the angle of attack and the configuration of wing on the aerodynamic characteristics of wingwas analyzed. |
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