Page 85 - Aerodynamics for Engineering Students
P. 85

68  Aerodynamics for Engineering Students

              Therefore, true air speed = Ma = 0.728 x 340.3
                                         248 m s-'  = 89 1 km h-'
                In this example, ~7 = 1 and therefore there is no effect due to density, Le. the difference is due
              entirely to compressibility. Thus it is seen that neglecting compressibility in the calibration has
              led the air-speed indicator to overestimate the true air speed by 59 km h-'  .


                 2,4  Two-dimensional flow

              Consider flow in two dimensions only. The flow is the same as that between two planes set
              parallel and a little distance apart. The fluid can then flow in any direction between and
              parallel to the planes but not at right angles to them. This means that in the subsequent
              mathematics there are only two space variables, x and y  in Cartesian (or rectangular)
              coordinates or r and 0 in polar coordinates. For convenience, a unit length of the flow
              field is assumed in the z direction perpendicular to x and y. This simplifies the treatment
              of two-dimensional flow problems, but care must be taken in the matter of units.
                In practice if two-dimensional flow is to be simulated experimentally, the method
              of constraining  the flow between two close parallel plates is  often used, e.g. small
              smoke tunnels and some high-speed tunnels.
                To  summarize, two-dimensional  flow is  fluid  motion  where  the  velocity  at  all
              points is parallel to a given plane.
                We have already seen how the principles of conservation of mass and momentum
              can  be  applied  to  one-dimensional  flows  to  give  the  continuity  and  momentum
              equations  (see  Section  2.2).  We  will  now  derive  the  governing  equations  for
              two-dimensional flow. These are  obtained  by  applying conservation  of  mass  and
              momentum to an infinitesimal rectangular control volume - see Fig. 2.8.

              2.4.1  Component velocities
              In general the local velocity in a flow is inclined to the reference axes Ox, Oy and it is
              usual to resolve the velocity vector ?(magnitude q) into two components mutually at
              right-angles.
























              Fig. 2.8 An  infinitesimal control volume  in a typical two-dimensional  flow field
   80   81   82   83   84   85   86   87   88   89   90