Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay

Figure 6

Mode shape and the corresponding frequency of the AGARD445.6 wing at the first four principal modes: (a) first mode at the frequency of 9.73 Hz; (b) second mode at the frequency of 37.54 Hz; (c) third mode at the frequency of 49.62 Hz; (d) fourth mode at the frequency of 92.37 Hz.

(a)

(b)

(c)

(d)