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
“…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
Horizontal T-foils allow for maximum lift generation within a given span. However, the lift force on a T-foil acts on the symmetry plane of the hull, thereby producing no righting moment. It results in a lack of transverse stability during foil-borne sailing. In this paper, we propose a system, where the height-regulating flap on the trailing edge of the foil is split into a port and a starboard part, whose deflection angles are adjusted to shift the centre of effort of the lift force. Similar to the ailerons which help in steering aircraft, the split-flaps produce an additional righting moment for stabilizing the boat. The improved stability comes, however, at a cost of additional induced resistance.
To investigate the performance of the split-flap system a new Dynamic Velocity Prediction Program (DVPP) is developed. Since it is very important for the performance evaluation of the proposed system it is described in some detail in the paper. A complicated effect to model in the DVPP is the flow in the slot between the two flaps and the induced resistance due to the generated vorticity. Therefore, a detailed CFD investigation is carried out to validate a model for the resistance due to the slot effect.
Two applications of the split-flap system: an Automated Heel Stability System (AHSS) and a manual offset system for performance increase are studied using a DVPP for a custom-made double-handed skiff. It is shown that the AHSS system can assist the sailors while stabilizing the boat during unsteady wind conditions.
The manual offset enables the sailors to adjust the difference between the deflection angles of the two flaps while sailing, thus creating a righting moment whenever required. Such a system would be an advantage whilst sailing with a windward heel. Due to the additional righting moment from the manual offset system, the sails could be less depowered by the sailors resulting in a faster boat despite the additional induced resistance.
It is shown in the paper that the control systems for the ride height and the heel stability need to be decoupled. The paper ends with a description of a mechanical system that satisfies this requirement.
“…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
Horizontal T-foils allow for maximum lift generation within a given span. However, the lift force on a T-foil acts on the symmetry plane of the hull, thereby producing no righting moment. It results in a lack of transverse stability during foil-borne sailing. In this paper, we propose a system, where the height-regulating flap on the trailing edge of the foil is split into a port and a starboard part, whose deflection angles are adjusted to shift the centre of effort of the lift force. Similar to the ailerons which help in steering aircraft, the split-flaps produce an additional righting moment for stabilizing the boat. The improved stability comes, however, at a cost of additional induced resistance.
To investigate the performance of the split-flap system a new Dynamic Velocity Prediction Program (DVPP) is developed. Since it is very important for the performance evaluation of the proposed system it is described in some detail in the paper. A complicated effect to model in the DVPP is the flow in the slot between the two flaps and the induced resistance due to the generated vorticity. Therefore, a detailed CFD investigation is carried out to validate a model for the resistance due to the slot effect.
Two applications of the split-flap system: an Automated Heel Stability System (AHSS) and a manual offset system for performance increase are studied using a DVPP for a custom-made double-handed skiff. It is shown that the AHSS system can assist the sailors while stabilizing the boat during unsteady wind conditions.
The manual offset enables the sailors to adjust the difference between the deflection angles of the two flaps while sailing, thus creating a righting moment whenever required. Such a system would be an advantage whilst sailing with a windward heel. Due to the additional righting moment from the manual offset system, the sails could be less depowered by the sailors resulting in a faster boat despite the additional induced resistance.
It is shown in the paper that the control systems for the ride height and the heel stability need to be decoupled. The paper ends with a description of a mechanical system that satisfies this requirement.
“…( 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%
“…Therefore Typhoon is provided with a Newton-Rhapson algorithm which alters the position and orientation of the vessel iteratively and, provided a good initial guess, will end up in an approximate equilibrium point. This algorithm is also explained in the work by Bagué et al [1]. The basic idea of this algorithm is that it changes the position of the vessel making use of a linear extrapolation of the forces which it wants to be zero.…”
Section: Static Equilibriummentioning
confidence: 99%
“…A more profound explanation of the DSA for aircrafts and the linearization of the system can be found in the work by Drela [2]. The DSA especially for hydrofoil crafts is explained in the work by Masuyama [4] or more recently by Bagué et al [1] where a framework is laid out to perform this DSA.…”
In this paper an open-source implementation of the vortex-lattice method to perform a dynamic stability analysis for hydrofoil crafts is discussed. The difference with existing vortex-lattice codes is the addition of a free-surface boundary condition which is needed to analyse surface piercing foils. This code, called Typhoon, can be used to perform a dynamic stability analysis (DSA) on hydrofoil vessels. The goal of this code is to have an easy-to-use and cheap alternative to compare different designs in early design stages. This paper gives a brief background to all the concepts used, followed by a short theoretical explanation of the vortex-lattice method. The second part of this paper focuses on a practical example of how this code can be used on an example.
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