Page 248 - Introduction to Naval Architecture
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PROPULSION                         233

        model tests. The model is fitted with propellers which are driven through
        a dynamometer which registers the shaft thrust, torque and revolutions.
        With the model being towed along the tank at its corresponding speed
        for the ship speed under study, the propellers are run at a range of
        revolutions straddling the self-propulsion point for the model. The
        model would already have been run without propellers to find its
        resistance. Data from the test can be plotted as in Figure 9.16.
          The self-propulsion point for the model is the point at which the
        propeller thrust equals the model resistance with propellers fitted. The
        difference between this resistance, or thrust, and the resistance of the
        model alone, is the augment of resistance or thrust deduction.



















        Figure 9.16 Wake and thrust deduction



          The propeller is now run in open water and the value of advance
        coefficient corresponding to the thrust needed to drive the model is
        determined. This leads to the average flow velocity through the
        propeller which can be compared to the ship speed corresponding to
        the self-propulsion point. The difference between the two speeds is the
        wake assuming an uniform distribution across the propeller disc. The
        difference in performance due to the wake variation across the disc is
        given by relative rotative efficiency which is the ratio of the torques
        needed to drive the propeller in open water and behind the model at
        the revolutions for self-propulsion.
          Although the propellers used in these experiments are made as
        representative as possible of the actual design, they are small. The
        thrust and torque obtained are not accurate enough to use directly.
        The hull efficiency elements obtained are used with methodical series
        data or specific cavitation tunnel tests to produce the propeller
        design.
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