Sensitivity Analysis of a CPAM Inverse Algorithm for Composite Laminates Characterization

Table 5

Natural frequencies of the aluminum and carbon/epoxy plates obtained by ABAQUS solver.

Frequencies
Aluminum
A1	115	166	218	292	307	500
A2	40	91	240	266	340	556
Carbon/epoxy
B1	61	84	150	230	231	261
B2	113	216	304	314	378	560
C1	100	306	338	360	381	600
C2	181	370	529	865	938	1033
D1	1661	3478	3855	4368	5059	6243	8769	9830	1029	10959
D2	1238	2169	3315	5320	6844	7015	7561	8910	10986	11650