Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay

Figure 10

Contour plots of pressure field for the Mach numbers of 0.8 (left frames, I) and 1.2 (right frames, II) at four different times: (a) 0.0 s; (b) 0.05 s; (c) 0.1 s; (d) 0.2 s.