Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay

Figure 9

Mode shapes of the elastic model at the first four vibration modes: (a) the first mode at the frequency of 19.01 Hz; (b) the second mode at the frequency of 19.03 Hz; (c) the third mode at the frequency of 54.86 Hz; (d) the fourth mode at the frequency of 54.91 Hz.

(a)

(b)

(c)

(d)