“…Previous research has shown that the Strouhal number is the principal parameter governing thrust generation and wake dynamics (Triantafyllou et al, 1991;Ramamurti & Sandberg, 2001). The ideal operating range in terms of thrust and efficiency has been found to be between St = 0.2 to 0.4, with pitch amplitudes between 40 • and 60 • , which has been demonstrated experimentally (Fish, 1998;Anderson et al, 1998;Read et al, 2003;Hover et al, 2004;Schouveiler et al, 2005;Techet, 2007) and computationally (Tuncer & Platzer, 1996;Jones & Platzer, 1997; Young & S. Lai, 2004;Xiao & Liao, 2010;La Mantia & Dabnichki, 2011;Mattheijssens et al, 2013). The effect of heave amplitude has received less attention, but typical values range from h 0 /c = 0.5 to 1.…”