“…In the first group (Figure 2(a)), load resultants are applied directly to a small number of sections of the blade, either through a master node which controls the whole section displacement by relations between nodes degrees of freedom (Forcier and Joncas, 2011; Haselbach et al, 2016; Joncas, 2010) or directly onto one (Griffith and Ashwill, 2011; Shokrieh and Rafiee, 2006) or a small number (Lindgaard and Lund, 2010; Lund and Stegmann, 2005) of nodes of the section of the shell FEM. This group consists of approaches where load resultant is applied at the blade tip or at the end of the studied segment (Haselbach et al, 2016; Lindgaard and Lund, 2010; Lund and Stegmann, 2005), and approaches where loads computed at different sections of the blade are applied onto the section where they had been computed (Griffith and Ashwill, 2011; Li et al, 2013; Shokrieh and Rafiee, 2006).…”