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26                                                          1.  Introduction


         provide  additional  research  capability  for  measuring  component  drag  through
         selective  deicing. The  aircraft  is equipped  with  several standard  instruments  for
         measuring  icing  cloud  properties.
            Wing  leading  edge  ice shapes  are  measured  in  flight  with  a  stereo  photogra-
         phy  system.  Wing  section  drag  is measured  with  a  wake  survey  probe  mounted
         on  the  wing  behind  the  region  where  the  stereo  photos  are  taken.  A  noseboom
         is  used  to  measure  airspeed,  angle-of-attack,  and  sideslip.  A  flight  test  system
         measures  flight  dynamics  along  a  flight  path.  The  system  includes  a  data  ac-
         quisition  system  and  an  inertial  package  that  contains  rate  gyros,  directional
         gyros,  and  servo  accelerometers.
            Subsection  1.4.1  describes the  calculation  of ice shapes  on the  lifting  surfaces
         of  this  aircraft,  and  subsection  1.4.2  describes  the  calculation  of  aerodynamic
         performance  characteristics  of  this  aircraft,  including  the  icing  effects.  In  both
         subsections  calculated  results  are  presented  and  compared  with  experimental
         data  to  demonstrate  the  efficiency  and  accuracy  of  each  calculation  method.


         1.4.1  Prediction  of  Ice  Shapes

         The  prediction  of  ice shapes  requires  knowledge  of aerodynamics  and  also  of  the
        physics  of  ice accretion. The nature  of the  ice depends  on meteorological  param-
        eters;  glaze  ice  is formed  at  temperatures  slightly  below  freezing  and  rime  ice  is
        increasingly  superimposed  as the  temperature  decreases.  Glaze  ice  is  character-
         ized  by  its  buildup  to  large  dimensions,  as  for  example  in  the  familiar  "horns"
         (Fig.  1.26a),  and  rime  ice  by  its  opaque  appearance  with  fine-grained  surface,
        see  Fig.  1.26b. The  shape  of the  ice  changes  with  time  and  is  influenced  by  the
         nature  of the  water  droplets  and  ice particles  which  impinge  on the  body  or  are
        carried  past  it, depending  upon their  size and the  flow properties  which,  in  turn,
        depend  upon the shape  of the body. The resulting impingement,  coalescence  and
         accretion  depend  on  the  temperatures  of  the  surface  and  of  the  discrete  and


















         (a)                                    (b)
         Fig.  1.26.  (a)  Glaze  and  (b)  rime  ice  shapes.
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