2011
DOI: 10.1016/j.enganabound.2010.09.009
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Influence of the wake model on the thrust of oscillating foil

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Cited by 22 publications
(3 citation statements)
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“…Related research has been conducted aiming at the problem. However, the foils were usually modeled in two dimensions or simplified to simple three-dimensional shapes [26][27][28]. Li et al mainly studied the wake topology of forked and unforked fish-like plate with numerical method [10].…”
Section: Introductionmentioning
confidence: 99%
“…Related research has been conducted aiming at the problem. However, the foils were usually modeled in two dimensions or simplified to simple three-dimensional shapes [26][27][28]. Li et al mainly studied the wake topology of forked and unforked fish-like plate with numerical method [10].…”
Section: Introductionmentioning
confidence: 99%
“…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.…”
Section: Introductionmentioning
confidence: 73%
“…It has to be discussed whether the Kutta condition can be applied in the unsteady flexible propeller BEM model because the Kutta condition was proposed solely for steady flows [22]. Later, the Kutta condition has been modified for unsteady models, which had been questioned [23].…”
Section: The Kutta Condition For Flexible Propellersmentioning
confidence: 99%