Page 264 - Practical Ship Design
P. 264

222                                                             Chapter 7

             7.5.5 Propeller design


             The author wanted to include in this book approximate formula that would enable a
             naval architect deprived of any other data to make a complete initial design, but has
             decided to admit defeat with propeller open water efficiency. The subject appears
             to be  too  complex  for any  simplified  treatment  and readers  are referred  to the
             standard text books on this subject.
               Fortunately, there is rarely any need to consider open water efficiency  at the
             initial design stage as Emerson’s QPC formula seems to fill the immediate need in
             power estimation with reasonable accuracy, enabling open water efficiency to be
             dealt with by propeller designers at a later stage.


             7.5.6 EfJiciency of a controllable pitch propeller


             The efficiency of a controllable pitch propeller is generally I-2%  less than that of a
             fixed pitch propeller for the same design condition - this being mainly due to the
             much larger boss diameter.
                If, however, there is a requirement for extensive operation at either a speed or a
             displacement significantly different from the design condition a controllable pitch
             propeller can offer substantial  advantages in fuel economy  and/or  speed at the
             second operating condition.



                                      7.6 HULL EFFICIENCY

             If it is impracticable to include in this book a satisfactory way of estimating open
             water efficiency, there is no point in giving formulae for hull efficiency as it is only
             the product of these - the QPC - which is of real interest. It is, however, worth
             discussing the components of hull efficiency to try to identify whether these can be
             influenced in the design process in a way that will improve powering efficiency.
                It will be recalled that:




             where
                     I-t          T-R            v -v,
                qh =-      and  t=-      and  w, =-
                    1-w,            T              V
             To optimise qd, the  thrust  deduction t  should  be  minimised,  the  Taylor wake
             fraction w, should be maximised as should the relative rotative efficiency q,.
   259   260   261   262   263   264   265   266   267   268   269