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2021
DOI: 10.5957/jst/2021.6.1.58
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Dynamic Stability Analysis of a Hydrofoiling Sailing Boat using CFD

Abstract: Abstract. This paper describes the study of the dynamic stability of a hydrofoiling sailing boat called the “Goodall Design Foiling Viper”. The goal of Goodall Design is to make hydrofoiling accessible to a wider public, whereas it was previously reserved for professional sailors at the highest level of the sport. To allow for safe operation, stability is an essential characteristic of the boat. The aim of this work is to find a strategy to perform a dynamic stability analysis using computational fluid dynamic… Show more

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Cited by 7 publications
(6 citation statements)
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“…During calculations of the stability derivatives, several assumptions were made to reduce the order of the equations, thereby reducing the accuracy of the method. Hence, Bagué et al (2021) used CFD to compute the stability derivatives for a foiling catamaran rather than the semi-empirical methods used by Masuyama. Though the stability derivatives provide data regarding the stability of the boat, dynamic simulations like disturbances and manoeuvring could not be studied.…”
Section: Dvpps Versus Linearized Approachesmentioning
confidence: 99%
“…During calculations of the stability derivatives, several assumptions were made to reduce the order of the equations, thereby reducing the accuracy of the method. Hence, Bagué et al (2021) used CFD to compute the stability derivatives for a foiling catamaran rather than the semi-empirical methods used by Masuyama. Though the stability derivatives provide data regarding the stability of the boat, dynamic simulations like disturbances and manoeuvring could not be studied.…”
Section: Dvpps Versus Linearized Approachesmentioning
confidence: 99%
“…( 1) the left hand side of the equation is the time derivative of the state-vector. The meaning of this state-vector is explained in more detail in the work by Bagué et al [1], but for this discussion it suffices to understand that it exists out of the change in forward speed u, change in fleight height z, change in trim angle θ , change in vertical speed…”
Section: Dynamic Stabilitymentioning
confidence: 99%
“…w and change in pitch velocity p. The longitudinal stability matrix [A] allows us to write this formula in a more convenient format, and it is this matrix which determines the dynamical behaviour. For a more thorough background on this particular case we refer to Bagué et al [1] and for a more general background to the dynamic stability analysis (of aeroplanes) we refer to Drela [2]. Apart from the mass and the mass-moment of inertia the stability matrix gets influenced by the so-called force and moment derivatives which originate from the afore mentioned substitution by the Taylor expansion of both the force and moment equations.…”
Section: Dynamic Stabilitymentioning
confidence: 99%
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