Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay

Figure 13

Temporal variation of the linear and angular displacements for the rigid and elastic models for the Mach number of 1.5 at different flight altitudes: (a) X-component displacement; (b) vertical displacement; (c) lateral displacement; (d) pitch angle displacement; (e) yaw angle displacement; (f) roll angle displacement.

(a)

(b)

(c)

(d)

(e)

(f)