Sketch the velocity distributions at the throat section (of diameter 2cm) and at the inlet of the venturimeter (of diameter 4cm).
cross section area of the throat at = 12 =
cross section area of the inlet ain = *22 = 4
vi and vt are the velocities at the inlet and throat
( volume of the fluid incoming = volume of fluid out going, when there are no sinks or no sources. There are no sources or sinks between the inlet and the throat)
using continuity eq. ain * vi = at *vt
vt = 4 vi
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