Consider the flow of air through a convergent-divergent duct, such as the venturi tube described in Prob. 4.4. The inlet, throat, and exit areas are 3,1.5, and 2 m2, respectively. The inlet and exit pressures are 1.02 × 105 and 1.00 × 105 N/m2, respectively. Calculate the flow velocity at the throat. Assume incompressible flow with standard sea-level density.
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