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56 Fundamentals of Ocean Renewable Energy


            Eq. (3.11) describes a vector, which is orientated towards the centre of the
                                             2
            earth, with a magnitude of R E Ω 2  = u /R E , which is called the centripetal
            acceleration.
               In order to apply the equations of motion in a rotating frame attached to the
            Earth, we need to find the relationship between rotating and nonrotating frames.
            In general, an object can rotate around three axes in space; therefore, to deal with
            a rotational coordinate system in a more general way, we need to formulate a
            relationship between inertial and rotational frames of reference in 3D. Consider
            a frame of reference at the centre of the Earth (inertial), and a rotational frame of
            reference at a point in the ocean (rotates around the Earth’s axis). The rotating
            frame may be described by three unit vectors, ˆ i r , ˆ j r , and k r . These unit vectors
                                                          ˆ
            are rotating with angular velocity   Ω around the inertial frame of reference. If
            we represent the position of an object in 3D using the position vector R,the
            rotational speed will be RΩ, or angular velocity will be   Ω × R. Based on the
            theory of relative motion in dynamics, for any vector variable A, we can write

                                dA         dA

                                       =         +   Ω × A             (3.12)
                                 dt         dt
                                    iner       rot
               Consequently, the relationship between velocities in the inertial and rotating
            frame can be written as


                    dR        dR
                           =         +   Ω × R ⇒ u iner = u rot +   Ω × R  (3.13)
                    dt  iner   dt  rot
               Similarly, if we apply Eq. (3.12) for acceleration (as a vector), it leads to


                             du iner      du iner

                                      =           + Ω × u iner         (3.14)
                               dt           dt
                                   iner         rot

               Because, u iner = u rot + Ω × R, therefore,


                du iner      d(u rot +   Ω × R)
                         =                    +   Ω × (u rot +   Ω × R)  (3.15)
                 dt   iner         dt       rot


                             du rot                              D   Ω

                         =           + 2   Ω × u rot + Ω × (   Ω × R) +  × R
                              dt                                  dt
                                   rot
                                                                       (3.16)
            As can be seen, the acceleration, which is observed in a rotational frame (i.e.
            du rot  ), is different from the acceleration, which is observed in an inertial frame
             dt
            (i.e.  du iner  ). The difference between these accelerations includes three terms:
                 dt
            Coriolis acceleration (−2Ω ×u rot ), the centripetal acceleration −Ω ×(Ω × r),



            and, Euler acceleration, the acceleration due to change in the angular velocity
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