This paper presents the results of computations of wave loads on fixed antifloating structures using three-dimensional, sink-source techniques (diffraction theory). Theoretical calculations are compared with model experiments. Statistical methods are discussed also. Introduction Basic contributions to the use of three-dimensional diffraction theory are the studies of Lebreton and Cormault and Garrison and Seetharama Rao. Since their presentations, this method increasingly has become the predominant technique for handling wave-induced loads on large offshore structures of arbitrary form. However, strip theories based on two-dimensional (diffraction) solutions have been applied in ship design to determine responses in regular waves for some time. The linear superposition technique proposed by St. Denis and Pierson normally is used to determine the responses in irregular seas. Different computer programs have been developed on the basis of the method proposed by Lebreton and Cormault. This paper presents the applications of a computer program and information gained from experimental program and information gained from experimental results. Computations of short-term responses in irregular seas using different wave-spectrum formulations are included also. This procedure has not been prominent in the design of large offshore structures yet, although it long has been used widely in ship design. Theoretical Formulation A review of the basic equations used in the diffraction theory program is presented in the following section. The Equations of Motions The motions of a floating structure are derived from the condition of dynamic equilibrium between excitation and restoring and the damping and inertial reactions of the system. Assuming that the system is harmonic, the six coupled linear differential equations of motions may be written as 6 -iwt (mjl + mjl) nl + Wjl nl + Cjl Nl = Fje. l=1 .................................(1) Here, mj is the component of the generalized mass matrix (j=l = 1,2, . . . 6) and mjl and Wjl are the added-mass and damping coefficients, respectively. The restoring coefficients Cjl and the complex amplitude of the exciting forces and moments are Fj. The real part should be used in all expressions where e-iwt is part should be used in all expressions where e-iwt is involved. The wave encounter frequency that is the same as the response frequency is denoted as w. Displacements are represented by n. Dots are used to indicate time derivatives. A right-handed coordinate system (x, y, z) fixed with respect to the mean position of the structure with an origin in the plane of the free undisturbed surface is presented. The coordinate z points up vertically through the center of gravity and the coordinate x points in the direction of backward motion. It is assumed that the structure is symmetric about the x-z plane and the center of gravity is located in (O, O, Zc). JPT P. 549
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