Skip to main content
. 2015 Apr;137(4):0410061–04100614. doi: 10.1115/1.4029430

Fig. 5.

Fig. 5

(a) Representation of the single element used to calculate the MA. The fiber structure was described using a single WAXS measurement. A biaxial stretch corresponding to the average strain measured in Coudrillier et al. [18] was applied on the ef and ep faces. (b) Representation of the Green–Lagrange strain/Cauchy stress response. The MA was calculated using Eq. (9).