The design of a cruise missile wing is a multidisciplinary work because the wing has to provide enough aerodynamic forces while being structurally in safe. Various parameters of the wing are investigated during the design phase in order to meet the design goals and achieve a successful design. In this paper, the effects of different parameters on the lift force and flutter speed of a cruise missile wing are presented. The aerodynamic analyses for predicting the lift force are performed by using FLUENT and the aeroelastic analyses for the determination of the flutter speed are conducted by using ZAERO
