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Main elements of a standard S.W.A.T.H. vessel

Main elements of a standard S.W.A.T.H. vessel

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Article
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The paper illustrates the main theoretical and computational aspects of an automatic computer based procedure for the parametric shape optimization of a particular unconventional hull typology: that for a catamaran S.W.A.T.H. ship. The goal of the integrated computational procedure is to find the best shape of the submerged hulls of a new U.S.V. (U...

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... of selecting the variation of the hull form is still based on a trial and error scheme, highly reliant on an expert evaluation and interpretation of C.F.D. results, which does not facilitate the convergence on the optimal solution. Small Waterplane Area Twin Hull (S.W.A.T.H.) ships are a special concept of hull typology and configuration (see Fig. 1) featuring two or more slender struts that are actually piercing the free surface, while the major part of the displaced volume is concentrated well below the free surface in torpedo-like underwater bodies. The major advantage of this hull typology is its superior seakeeping ability. Another benefit of this type of vessel is a high ...
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... order to have an excellent fitting between the hull surface modeled inside the C.A.D. software and the discretized one for the computation, it has been divided into 9 different zones, as shown in Fig. 10: one for each side of the two struts and five for the submerged ...
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... regards free surface it has been divided in two zones, as shown in Fig. 11: the first one from the symmetry plane to the waterline of the hull and the other one from the end of the first to the end of the computational domain. ...
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... care has to be paid on the selection of valid points: in fact, as particularly evident from Fig. 12, there are few dozen of points which fall well below the mean trend line traced by the others: these points correspond to fake calculations, in which the C.F.D. solver has predicted an unrealistically low value of the objective function, generally due to a mis-generated panel mesh discretization of the hull geometry. The check of these ...
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... hence a higher wave resistance, the predicted wavy free surface elevation can be compared from one case to another. With this simple criteria often used by designers in trial and error procedures it is possible to visually guess which solution could be better than others on the basis of the free wave pattern colored contours as those presented in Fig. 15 to Fig.17. Differences in the generated wave pattern by two different hull shapes, at a given speed, are justified by the interference effects that each wave train generated along the hull has with the other. In order to realize the effectiveness of the optimization procedure, both initial (first point created by Sobol D.o.E.) and ...
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... content and hence a higher wave resistance, the predicted wavy free surface elevation can be compared from one case to another. With this simple criteria often used by designers in trial and error procedures it is possible to visually guess which solution could be better than others on the basis of the free wave pattern colored contours as those presented in Fig. 15 to Fig.17. Differences in the generated wave pattern by two different hull shapes, at a given speed, are justified by the interference effects that each wave train generated along the hull has with the other. ...
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... of the optimization procedure, both initial (first point created by Sobol D.o.E.) and optimized hull variants are compared against a conventional (drop-shaped) underwater hull form, whose profile resembles the shape of a N.A.C.A. four digits symmetric airfoil, with maximum thickness at about 30% of chord length from the leading edge. Fig. 14 presents the 3D panel mesh generated for the compared hull shapes. Their wave patterns are compared from Fig. 15 to Fig. 17. Table 4 resumes the main features of the four design ...
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... variants are compared against a conventional (drop-shaped) underwater hull form, whose profile resembles the shape of a N.A.C.A. four digits symmetric airfoil, with maximum thickness at about 30% of chord length from the leading edge. Fig. 14 presents the 3D panel mesh generated for the compared hull shapes. Their wave patterns are compared from Fig. 15 to Fig. 17. Table 4 resumes the main features of the four design ...

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... Examples of direct modification includes Beizer curve [11], non-uniform rational basis spline-NURBS [17,18] and T-splines [12]. Some examples of systematic variation methods applied in hull form optimisation include Lackenby shift [19], parametric modification [20,21] and free-form deformation [22]. ...
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... BM KB KG    (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14) Where: ...
... L BM --longitudinal metacentric radius KB --height of center of buoyancy to base line KG --Height of the Center of Gravity to the Baseline As it's known: (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15) In normal circumstances, the form of main cross section is assumed to be an ellipse, and the vertical direction radius ...
... By Equation (2-13) ~ (2-16), the second moment of the strut waterplane area is: (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18) The distance between the buoyant centre of the hull and the first endpoint is cb L : (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18)(19) Where S c is the vertical distance of cross section between the hull and the strut (see Figure (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18)(19)(20) Thus, by Equation (2)(3)(4)(5)(6)(7)(8) and (2)(3)(4)(5)(6)(7)(8)(9)(10)(11)(12)(13)(14)(15)(16)(17)(18)(19), B M it can be expressed as: ...
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