Research Article

Static and Vibrational Analysis of Partially Composite Beams Using the Weak-Form Quadrature Element Method

Figure 8

First five mode shapes of SS composite beam for 𝛼 𝐿 = 2 and 𝛼 𝐿 = 3 0 .
974023.fig.008a
(a) Longitudinal mode shape 𝛼 𝐿 = 2
974023.fig.008b
(b) Longitudinal mode shape 𝛼 𝐿 = 3 0
974023.fig.008c
(c) Flexural mode shape 𝛼 𝐿 = 2
974023.fig.008d
(d) Flexural mode shape 𝛼 𝐿 = 3 0