Page 137 - Theory and Design of Air Cushion Craft
P. 137

drag
                                                               drag
                         Total
                                                        Friction
                                                                            Method
                  Remarks
                                             sidewalls
                                                 sidewalls
                                                      sidewalls
                                                                                Table 3.3
                         drag
                                                                     Drag items
                                        Appendage
                                 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
                                             g) where C w is
                                                                                Methods for calculating the drag of
                                              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
                                                        BJ(p w
                                                      3.2 and
                         + R
                                        be obtained
                                                        g)
                                  I D
                                              R^ is included in R,
                                                      3.3
                                      boats
                                        by the
                                  +/ ?
                                                                 /? a
                                                             R m
                                                   R^f
                                                                           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
                       + ^
                                             B c)l( Pvi
                                                                            Method 4
                  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
                trim angle then use C sk as
                  is at optimum
                                             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
                                                   approx
                               =s a ^
                                                      Fig. 3.4
                                      sidewalls is included in
                         + R m +
                                 B e p c v
                              =s b «
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