
144 Industrial Air Quality and Ventilation
© 2010 Taylor & Francis Group, LLC
would result from Equation 4.71 by integrating all summands over the cross-section
of the jet with the following boundary conditions:
y
y
x
=
000,
at (4.75)
y
x
x
=
∞00,
at (4.76)
The integral relation would be similar for an axially symmetric jet:
=− −
()
−
∫
x
urdr vu vurdr
x
rdr
xx
n
x
2
.. (4.77)
4.1.2 struCture of aIr streams In a flat jet of loose matter
4.1.2.1 Self-Similar Motion Equations
With the purpose of determining the velocity eld and streamlines in a jet of injected
air, we shall resort to the afne transformation method accepted i ...