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         4  RESULTS
         The  flowfields around  the  underwater  axisymmetric  bodies  with  full  appendages are computed as
         steady-state solutions  to the  incompressible Navier-Stokes equations. The  full  appendages  include  a
         fairwater  and  four  stem  appendages.  The  numerical  velocity distribution and  nominal  wake  at  the
         propeller are compared with the experiment data measured in the wind tunnel. The Reynolds number in
         the calculation and experiment are  6.0~ IO6.  The complete calculation was carried out by two steps.
         The flowfields around the body and a fariwater are numerically simulated firstly, which can provide the
         inlet boundary condition for the following fine simulation of flowfield around stem part of body and four
         stem appendages.
         The  numerical  dimensionless  circumferential-mean velocity  along  the  radius  of  the  propeller  are
         presented in Fig.  1, which are in good agreement with the experimental data. The details of numerical
         dimensionless circumferential-mean velocity and the experimental data can also been found in Table 1.
         Except few points, the relative error between the numerical results and the experimental data is less than
         3%, their average relative error is only 2.107%, the accurate numerical nominal wake at propeller can be
         used  as  input data  of  vehicle propdsor  blade design.  The numerical dimensionless circumferential
         velocity distribution at different radius station are showed in Fig. 2(a)-Fig.  2(g). There are difference
         between the numerical results and the experimental data, but their phases are similar, so the calculated
         circumferential velocity can be applied to the optimization and evaluation of hydrodynamics noise of
         vehicle propulsor. The code developed in this paper has been used in the design and optimization of new
         underwater bodies with full appendages.

                                          TABLE 1
                         COMPARISON OF NUMERICAL CIRCUMFERENTIAL VELOCITY
                                    WITH EXPERIMENTAL DATA
















         5  CONCLUSIONS

         Based on flux-splitting, implicit high-resolution schemes have been constructed for efficient calculations
         of steady-state solutions to the three dimensional, incompressible Navier-Stokes equations in curvilinear
         coordinates. The third-order-accurate efficient EN0 has been  applied in the calculations, which can
         capture  the  details  of the  flowfield  around underwater bodies with  full  appendages. The  numerical
         results agree quite well with the experimental data. The schemes and code developed in this paper can be
         applied  in the  design of underwater vehicle propulsor and  in the optimization and  evaluation of  its
         hydrodynamics noise. Also the code can be used in the optimization and design of shapes of vehicle
         body and its appendages.
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