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3. DESCRIPTION OF BEMUse

3.9 From potential to forces

Calculating the velocity potential is necessary for then being able to calculate the forces and pressures acting on the body. To get there, BEMUse uses the equations written in Chapter 2. In particular, the total pressure working on the surface of the body is calculated through the Bernoulli equation

𝑝(π‘₯ , 𝑑) = βˆ’πœŒ (πœ•πœ™

πœ•π‘‘ +1

2βˆ‡πœ™ βˆ™ βˆ‡πœ™ + 𝑔𝑧) (3.32)

There are although numerous other parameters of great interest when dealing with floating platforms and hydrodynamics in general.

3.9.1 Added mass and damping

First there is added mass, which is defined as the inertia added to a system because a body moves or deflects some volume of the fluid surrounding it when subjected to forces, thus accelerating and decelerating. Since it identifies inertia, it's expressed in π‘˜π‘” in the case of translational motions and π‘˜π‘” βˆ™ π‘š2 for rotational ones. In alternative added mass can also be expressed in dimensionless form, becoming the added mass coefficient. To obtain it, it’s sufficient to divide the added mass times the displaced fluid mass.

Then there is damping, which in physics is generally described as the influence on an oscillatory system which reduces, restricts or prevents its oscillation. Damping is directly proportional to the relative velocity between the two bodies (platform and water, in this case). In the case of fluids, we refer to radiation damping which is mostly due to the viscosity of the water. It is expressed in π‘˜π‘”/𝑠 for translational motions and in π‘˜π‘” βˆ™ π‘š2/𝑠for rotational ones. Also in this case, a dimensionless damping coefficient can be expressed as the ratio of the calculated damping and the mass of displaced water.

The added mass and damping are obtained integrating the value of the radiation potential over the body:

𝐴𝑖𝑗 βˆ’ 𝑖

πœ”π΅π‘–π‘— = ∬ π‘›π‘–πœ™π‘Ÿ,𝑗𝑑𝑆

𝑆

(3.33) Where the subscript i indicates the particular direction of the force and j the coordinate in which the surface oscillation occurs. A11, therefore, designates the x-forces caused by an oscillation in the x-direction. This kind of motion is commonly referred to as surge motion. In the y-direction it's called sway, and in z-direction it's heave. For rotational motions, rotation around the x-, y- and z-axis are called roll, pitch and yaw, respectively.

In WAMIT the non-dimensional added mass and damping coefficients are obtained as follows 𝐴̅𝑖𝑗 = 𝐴𝑖𝑗

πœŒπΏπ‘˜ 𝐡̅𝑖𝑗 = 𝐡𝑖𝑗

πœŒπΏπ‘˜πœ” (3.34 π‘Ž π‘Žπ‘›π‘‘ 𝑏)

Where k = 3 for both i, j being equal to 1, 2 or 3; k = 4 for i = 1, 2, 3 and j = 4, 5, 6 or i = 4, 5, 6 and j = 1, 2, 3; k = 5 for both i, j = 4, 5, 6.

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3.9.2 Exciting forces

The periodic forces on the body which arise due to the diffraction of the incoming harmonic wave are called exciting forces. To calculate them, the potential of the incoming wave is needed.

In the infinite-depth case, it’s expressed as πœ™πΌ = 𝑖𝑔𝐴

πœ” π‘’πœˆπ‘§π‘’π‘–πœˆ(π‘₯ π‘π‘œπ‘ π›½+π‘₯𝑦 𝑠𝑖𝑛𝛽) (3.35)

Where A is the wave’s amplitude, and Ξ² is its heading. Making use of Haskind relations for the diffraction potential, the forces can be expressed as a function of the radiation potential defined previously for the oscillating body:

𝑋𝐼 = βˆ’π‘–πœ”πœŒ ∬ (π‘›π‘–πœ™π‘– βˆ’πœ•πœ™π‘–

πœ•π‘› πœ™π‘—) 𝑑𝑆

𝑆

(3.36) This allows to avoid the calculation of the diffraction potential on the surface, but simply to manipulate the results of the radiation potential. The exciting forces differ according to the direction of the incoming waves. Therefore, the results obtained must always be expressed indicating the angle which they refer to. This angle is usually measured starting from the positive x-axis. In this text, an angle of 45Β° was always used.

Exciting forces are expressed in 𝑁/π‘š for translational motions and in π‘π‘š/π‘š for rotational ones, but they are also found in their non-dimensional form

𝑋̅𝑖 = 𝑋𝑖

πœŒπ‘”π΄πΏπ‘š (3.37)

Where m = 2 for i = 1, 2, 3 and m = 3 for i = 4, 5, 6.

3.9.3 Response Amplitude Operators

The Response Amplitude Operator, or RAO, is an indication of the degree of movement induced in a floating body due to a passing hydrodynamic wave. RAOs can be calculated for each degree of freedom of the body, both translational and rotational. Like the exciting force, the direction of the incoming wave must be defined. As before, 45Β° was always the choice. The formula used to calculate each RAO is taken from Baghfalaki, Das, and Das (2012) [28]:

𝑍𝑖(πœ”) =𝑋𝑖(πœ”)

𝐷𝑖 = 𝐹𝑖(πœ”)

βˆ’πœ”2(𝐴𝑖𝑖(πœ”) + 𝑀𝑖𝑖) + π‘–πœ”π΅π‘–π‘–(πœ”) + 𝐢𝑖𝑖 (3.38) Where Xk (Ο‰) is the motion in the frequency domain, and Dk is the corresponding wave amplitude. Fk is the exciting force, Akk is the value of added mass, Mkk the mass and inertia matrix, Bkk is the damping coefficient, Ckk is the value of the hydrostatic restoring matrix and Ο‰ is the frequency of the waves.

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The mass and inertia matrix contains the value of mass and rotational inertia of the body under inspection and is defined as

𝑀𝑖𝑖 =

[

π‘š 0 0 0 π‘šπ‘§π‘” βˆ’π‘šπ‘¦π‘”

0 π‘š 0 βˆ’π‘šπ‘§π‘” 0 π‘šπ‘₯𝑔

0 0 π‘š π‘šπ‘¦π‘” βˆ’π‘šπ‘₯𝑔 0

0 βˆ’π‘šπ‘§π‘” π‘šπ‘¦π‘” 𝐼π‘₯ βˆ’πΌπ‘₯𝑦 βˆ’πΌπ‘₯𝑧

βˆ’π‘šπ‘§π‘” 0 βˆ’π‘šπ‘₯𝑔 βˆ’πΌπ‘¦π‘₯ 𝐼𝑦 βˆ’πΌπ‘¦π‘§

βˆ’π‘šπ‘¦π‘” π‘šπ‘₯𝑔 0 βˆ’πΌπ‘§π‘₯ βˆ’πΌπ‘§π‘¦ 𝐼𝑧 ]

(3.39)

On the other hand, the hydrostatic restoring matrix is defined as follows in the WAMIT User Manual [29]

𝐢𝑖𝑖 = [

0 0 0 0 0 0

0 0 0 0 0 0

0 0 𝐢3,3 𝐢3,4 𝐢3,5 0 0 0 0 𝐢4,4 𝐢4,5 𝐢4,6

0 0 0 0 𝐢5,5 𝐢5,6

0 0 0 0 0 0 ]

(3.40)

Where

𝐢(3, 3) = πœŒπ‘” ∬ 𝑛3𝑑𝑆

𝑆𝑏

(3.41π‘Ž)

𝐢(3, 4) = πœŒπ‘” ∬ 𝑦𝑛3𝑑𝑆

𝑆𝑏

(3.41𝑏)

𝐢(3, 5) = βˆ’πœŒπ‘” ∬ π‘₯𝑛3𝑑𝑆

𝑆𝑏

(3.41𝑐)

𝐢(4, 4) = πœŒπ‘” ∬ 𝑦2𝑛3𝑑𝑆

𝑆𝑏

+ πœŒπ‘”π‘‰π‘§π‘βˆ’ π‘šπ‘”π‘§π‘” (3.41𝑑)

𝐢(4, 5) = βˆ’πœŒπ‘” ∬ π‘₯𝑦𝑛3𝑑𝑆

𝑆𝑏

(3.41𝑒)

𝐢(4, 6) = βˆ’πœŒπ‘”π‘‰π‘₯𝑏+ π‘šπ‘”π‘₯𝑔 (3.41𝑓)

𝐢(5, 5) = πœŒπ‘” ∬ π‘₯2𝑛3𝑑𝑆 + πœŒπ‘”π‘‰π‘§π‘βˆ’ π‘šπ‘”π‘§π‘”

𝑆𝑏

(3.41𝑔)

𝐢(5, 6) = βˆ’πœŒπ‘”π‘‰π‘¦π‘+ π‘šπ‘”π‘¦π‘” (3.41β„Ž)

V is the volume of the body, ρ is the density of the water, and m is the mass of the body. The coordinates with subscript b refer to the center of buoyancy of the body, the ones with subscript g to its center of mass.

To improve the computational performance of the software, the surface integrals are calculated as the discrete sum of the values on each panel. x and y are thus the coordinates of each centroid, and n is the vector normal to the surface, with its three components.

44 These values are then normalized as follows:

𝐢̅(3, 3) = 𝐢(3, 3) πœŒπ‘”πΏβ„ 2 (3.42π‘Ž)

𝐢̅(3, 4) = 𝐢(3, 4) πœŒπ‘”πΏβ„ 3 (3.42𝑏)

𝐢̅(3, 5) = 𝐢(3, 5) πœŒπ‘”πΏβ„ 3 (3.42𝑐)

𝐢̅(4, 4) = 𝐢(4, 4) πœŒπ‘”πΏβ„ 4 (3.42𝑑)

𝐢̅(4, 5) = 𝐢(4, 5) πœŒπ‘”πΏβ„ 4 (3.42𝑒)

𝐢̅(4, 6) = 𝐢(4, 6) πœŒπ‘”πΏβ„ 4 (3.42𝑓)

𝐢̅(5, 5) = 𝐢(5, 5) πœŒπ‘”πΏβ„ 4 (3.42𝑔)

𝐢̅(5, 6) = 𝐢(5, 6) πœŒπ‘”πΏβ„ 4 (3.42β„Ž)

Where L is the characteristic length of the body.

RAOs have the dimension of π‘š/π‘š for translational motions because they measure the ratio between the motion of the body and the amplitude of the wave, while rotational ones are expressed in Β°/π‘š, as they evaluate the ratio between the angular motion of the body and, again, the amplitude of the wave. As for the other parameters calculated, also RAOs have their non-dimensional form

𝑍̅𝑖 = 𝑍𝑖 𝐴 𝐿𝑛

(3.43) Where n = 0 for i = 1, 2, 3 and n = 1 for i = 4, 5, 6.

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