Calculate the flow velocity at the throat

Reference no: EM13250338

Consider the flow of air through a convergent-divergent duct. The inlet, throat and exit areas are 3.5, 1.75, and 2.25 m2 respectively. The inlet and exit pressures are 1.03x105 and 1.015x105 N/m2 respectively.

Calculate the flow velocity at the throat. Assume incompressible flow with sea-level density.

Reference no: EM13250338

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Calculate the flow velocity at the throat : Consider the flow of air through a convergent-divergent duct. The inlet, throat and exit areas are 3.5, 1.75, and 2.25 m2 respectively. The inlet and exit pressures are 1.03x105 and 1.015x105 N/m2 respectively.

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