9 Computer Simulation of the Process of Loss of Stability …
135
90
о
75
о
60
о
45
о
a
b
c
Fig. 9.5 Characteristic buckling forms of composite cylindrical shells under loading by external
pulse at a rate of 5 GPa/s for different reinforcement angles and intensity of axial compression:
N 0
11 = 0 (a), N 0
11 = 0, 45N ∗
11 (b) and N 0
11 = 0, 9N ∗
11 (c), respectively
135
90
о
75
о
60
о
45
о
a
b
c
Fig. 9.5 Characteristic buckling forms of composite cylindrical shells under loading by external
pulse at a rate of 5 GPa/s for different reinforcement angles and intensity of axial compression:
N 0
11 = 0 (a), N 0
11 = 0, 45N ∗
11 (b) and N 0
11 = 0, 9N ∗
11 (c), respectively