Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay

Figure 11

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

(a)

(b)

(c)

(d)

(e)

(f)