Page 180 - Theory and Design of Air Cushion Craft
P. 180

Calculation of ACV transverse stability  163

          Commentary
          It  has  been  shown by Blyth's test programme  that  the on-cushion stability of  an SES
          should  be principally assessed  in  relation  to  rolling behaviour  in synchronous  beam
          seas and  in relation  to  the hydrodynamic forces  developed  in high-speed  turns.
            In  a  seaway, capsizing  of  an  SES is most  probable  in  steepness-limited  beam  seas
          with  a  period  close  to  resonance.  An  alteration  in course  and/or  a  reduction  in  lift
          power  both  substantially  reduce  the  probability  of  capsize  occurring.  It  has  been
          shown  that  for  each  design,  there  is  a  VCG  below  which  capsizing  becomes
          improbable.
            In high-speed turns, the hitherto  unidentified possibility of large amplitude roll/yaw
          oscillations  occurring  has  been  detected  and  examined.  It  seems  probable  that  this
          behaviour  is associated  with a  zone  of  negative roll  stiffness  in turns,  created  by  the
          manner  in which hydrodynamic forces vary with roll attitude.



                               of ACV   transverse stability

          Introduction


          An ACV has no natural  restoring moment  from  the cushion  (plenum chamber) itself
          while  heeling  on  cushion.  Air jet  craft  derived  stability moments  from  the  increased
          force  of  the jet  on the downgoing  side and  reduced  force  on the upgoing side, though
          these were small and  so such craft  were very sensitive to movements of  craft  pay load.
            As an  ACV heels, due perhaps  to  the movement  to  one side of  a person  on board
          creating  an overturning moment,  a negative restoring moment  will act on the ACV if
          no  other  stability moments  are  created  by  deformation  of  the  peripheral  skirts,  as
          shown  in  Fig.  4.26.  This  is because  the  cushion  pressure  will  be the  same  across  the
          craft  width in the case  of  no cushion  compartmentation.
                                                                               has
            The skirt geometry and in the case of skirts with pressurized loops or bags, p\lp c
          a  strong  influence  on  the  righting moment  which  is  generated  for  an  ACV.  When
          travelling  over  water,  the  skirt  stiffness  will  then  affect  the  water  displaced  on  the
          downgoing  side, in  a similar way to  the  action  of  SES sidewalls, below hump  speed.
          Above hump  speed, the skirt surface presented  to the water acts as a planing surface,
          though  the  force  that  can  be  generated  is limited  to  that  which  can  be  transmitted
          around  the fabric membrane  back  to the craft's hard  structure.


          Cushion  compartmentation
          In  the case where an  ACV compartmented  longitudinally hovers statically on  a rigid
          surface,  cushion  pressure on  the  side heeling down  increases due to  reduced  air flow
          and the cushion pressure decreases for the other  side because of increased escape  area
          and  therefore flow rate.  Thus  the  different  cushion  pressures  give  a  direct  restoring
          moment,  moving the effective  centre of pressure to the downward  side of the craft,  as
          shown in Fig.  4.27.
            Meanwhile,  the  transverse component  of  P ci)smO  of  the  cushion  pressure  resultant
             will  also  lead  to  a  drifting  motion.  For  this  reason,  drifting  in  general  always
          P ce
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