Page 136 - Theory and Design of Air Cushion Craft
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drag
                                                               drag
                         Total
                                                        Friction
                                                                            Method
                                                      sidewalls
                                             sidewalls
                                                 sidewalls
                  Remarks
                                                                                Table 3.3
                         drag
                                        Appendage
                                                                     Drag items
                                 Skirt drag or
                                                           to air cushion
                                                        drag of
                                        drag
                                              Residual drag of
                                                        the
                                                                 Aerodynamic profile
                                 residual
                                                   Wetted surface area of
                                                             Wave-making drag due
                                             (p v
                                              R w
                               + R^
                                                                            Method
                               +
                              according
                                              = 0.05
                                                                            1
                                                                           Estimation
                                           Figs 3.2 and
                              to
                               7? sww
                                           3.3
                               +
                                              C w (pi
                                                                                Methods for calculating the drag of
                                             g) where C w is
                                              5 C)/
                              Fig. 3.19
                                             from
                               /?„„) or
                                                        /? w
                                                      from
                                                        =
                               WIW m
                                        R. dp can
                                                                            Method
                                                      Fig.
                                                                            2
                                                        C w pi
                                                                         model tests
                                                                                SES over calm water
                         R.
                                  ?
                                                                           Conversion from
                                      as for high-speed
                                                      3.2 and
                                                        BJ(p w
                         + R
                                        be obtained
                                                        g)
                                  I D
                                              R^ is included in R,
                                                      3.3
                                      boats
                                        by the
                                  +/ ?
                                                                 /? a
                                                   R^f
                                                             R m
                                                                           NPL
                                                                 =
                                                             =
                                                                            Method
                                                             p. A
                                  +/ ?
                                                                 0.5p
                                                   = (C {
                                                                            3
                                                             Q v
                                                                 C a
                                                        C w can be obtained
                                                                           Method
                                  +
                                        same methods
                                                                 S. A v
                                                   + AC f) S t q w
                  If
                                                   C f
                                             (pi
                                 ^sk
                                 =
                                              fl sww =
                                           is from
                               C sk from
                       + ^
                                                                            Method 4
                                             B c)l( Pvi
                  the craft
                                              0.05 C w
                       + ^
                                                   = 0.455 / [/ g
                                 Qk B, h,. # w
                               Fig. 3.17
              shown in Fig. 3.17,
                       +
                                           Figs 3.2 and
             otherwise increment.
                                                   Re] 2 ' 58
                                             g) where C w
                                           3.3
                  is at optimum
                trim angle then use C sk as
                                             Kf t
                                 R. k
                                                   AC f
                                                      g 4)
                                              /? sww
                                 =
                                                   =
                            0.0087
                                              =
                                             from
                                 (a
                                              Kf t
                                                                            Method 5
                                 +
                         +
                                                      C w from
                                              W
                                                   0.0004
                         R a
                               where 0.00225
                                    appendage drag
                                 b Fr d)
                                        Residual drag for
                              0.021, and 0.0015
                                                                           Kolezaev Method
                                             Fig. 3.30
                                                      Fig. 3.4
                                                   approx
                               =s a ^
                         + R m +
                                      sidewalls is included in
                                 B e p c v
                              =s b «
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