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             the towing carriage. Since the model “S” is not geometrically similar to the test boat and a small block
             is attached as shown in Figure 7 to make the bottom  of the model “S, on which air cavity forms,
             similar to  the  shape  of  the  test  boat.  The  flow rate  that  provides the  maximum  cavity area  is
             determined based on the procedure mentioned earlier and the results are summarized in Table 2.
                                     --  -



                                                I
                              Partition block for making a division
                 Figure 7: Body plan of the modified model “s” for estimating flow rates of air for the test boat

                                               TABLE 2
                            ESTIMATION OF CRITICAL FLOW RATES OF AIR FOR THE TEST BOAT
                                           Model (2 = 19.5)            Test boat
                 Fn,      e,, crtrtco1
                                      v  (&s)   Qm. cnrm/  (I /min)   V (kt~) QAv.  cnrtcal  (I /min)
                9.9814   Less than 0.0119   1.398   Less than 0.1   12   Less than 170
                13.3085  Less than 0.0089   1.864   Less than 0.1   16   Less than 170
                16.6356   0.0107-0.0143   2.330    0.15-0.2      20        250-340
                19.9627   0.0119-0.0149   2.796    0.2-0.25      24        340-420
                22.458  1   0.01 85-0.0212   3.145   0.35-0.4    27        590-670

             4  CONCLUSIONS
             Three geometrically similar models are made to investigate the scale law governing the air lubrication.
             Air is supplied behind a step placed on the bottom of the model and relations between flow rates of air
              and the shapes and areas of air cavity as well as the resistance reduction are observed.
              It is found that there exist critical flow rates of air for each Froude number above which no significant
              changes  in shape of  cavity or reductions in  the  resistance occur.  The critical rate and cavity area
              depend on the Froude number and scale effect is not dominant. If air is supplied above the critical rate,
             the shapes of air cavity generated on the geometrically similar models are also similar. If it is assumed
              that the wetted surface area decreases as much as air cavity area, conventional methods for resistance
              extrapolation may also be applied to the ship with air cavity.
              A test boat of 3.16m long is constructed to examine the practical applicability of the air lubrication and
              trials are going underway. The results will help understanding of scale law for air lubrication.

              References
              Bushnell D.M. and Heher J.N.  (Edited by) (1990). viscous Drag Reduction in Boundary Layers, The
              American Institute of Aeronautics, Inc., Washington, DC, USA
              Jang J. and Kim H. (1999). On the Reduction of a Ship Resistance by Attaching an Air Cavity to Its
              Flat Bottom, Journal of  the Sociery of Naval Architects of Korea, 36:2,1-8.
              Knapp R.T., Daily J.W.  and Hammitt F.G.  (1970). Cavitation, McGraw-Hill, USA
              Lewis E.V. (Edited by) (1988). Principles of  Naval Architecture Vol. ZZ, SNAME, USA
              Sat0 T., Nakata T., Takeshita M.,  Tsuchiya Y.  and Miyata H. (1997). Experimental Study on Friction
              Reduction of a Model Ship by Air Lubrication, Journal  of  the Society of Naval Architects of Japan,
              182, 121-128.
              Tanaka H.,  Nakato M.,  Nakatake K., Ueda T.  and Araki S. (1991). Cooperative Resistance Tests with
              Geosim Models of a High-speed Semi-Displacement Craft, Journal ofthe Society of Naval Architects
              of Japan, 169,55-64.
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