Page 276 - Introduction to Naval Architecture
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MANOEUVRING                         261

        The pull-out manoeuvre
                       1
        This manoeuvre  is also related to the directional stability of the ship.
        The rudder is put over to a certain angle and held until the ship is
        turning at a steady rate. The rudder is returned to amidships and the
        change in the turn rate with time is noted. For a stable ship the turn
        rate will reduce to zero and the ship takes up a new steady straight line
        course. A plot of the log of the rate of turn against time is a straight line
        after a short transition period. If the ship is unstable the turn rate will
        riot reduce to zero but there will remain some steady rate of turn. The
        area under the plot of turn rate against time gives the total heading
        change after the rudder angle is taken off. The smaller this is the more
        stable the ship.
          If the ship is conducting turning trials it will be in a state of steady
        turning at the end of the run. If the rudder is centred the pull-out
        manoeuvre can be carried out immediately for that speed and rudder
        angle.


        MANOEUVRING DEVICES
        Rudder forces and torques
        Rudder forces
        Rudders are streamlined to produce high lift with minimum drag. They
        are symmetrical to produce the same lift characteristics whichever way
        they are turned. The force on the rudder, F, depends upon the cross-
        sectional shape, area A, the velocity Vthrough the water and the angle
        of attack a.




        The constant depends upon the cross section and the rudder profile, in
        particular the ratio of the rudder depth to its chord length and the
        degree of rounding off on the lower corners. The lift is also sensitive to
        the clearance between the upper rudder surface and the hull. If this is
        very small the lift is augmented by the mirror image of the rudder in
        the hull. f(a) increases roughly linearly with a up to the stall angle
        which is typically about 35°. f(a) will then decrease.
          Various approximate formulae have been proposed for calculating F.
        An early one was:




        In this an allowance was made for the effect of the propeller race by
        multiplying Fby 1.3 for a rudder immediately behind a propeller and
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