134
N. A. Abrosimov et al.
90
о
75
о
60
о
45
о
a
b
c
Fig. 9.4 Characteristic buckling forms of composite cylindrical shells for different reinforcement
angles: under quasi-static loading (a); dynamic loading by external pressure pulse at the rates of
5 GPa/s (b) and 20 GPa/s (c) in combination with quasi-static compression intensity N 0
11 = 0, 9N ∗
11
N. A. Abrosimov et al.
90
о
75
о
60
о
45
о
a
b
c
Fig. 9.4 Characteristic buckling forms of composite cylindrical shells for different reinforcement
angles: under quasi-static loading (a); dynamic loading by external pressure pulse at the rates of
5 GPa/s (b) and 20 GPa/s (c) in combination with quasi-static compression intensity N 0
11 = 0, 9N ∗
11