Effect of Magnus Force on Spin Stabilized Missile in Normal Crosswind Conditions

When the missile is stabilized by its spin and geometry we considered for the missile is almost cylinder, which produces Magnus force when it experiences crosswind. The produced Magnus force create disturbances in its flight path or Magnus force can be used for Maneuvering purpose by finding the stable condition of the missile. This paper determines the Number of Rotation for which the Magnus force is Zero under normal crosswind conditio