Air flows steadily through a converging-diverging nozzle a mass flow rate of 3.00kg/s. The air enters the duct at a pressure of 1400kPa and a temperature of 200°C with a low velocity, and it expands in the nozzle to an exit pressure of 92kPa. The duct is designed so that the flow can be approximated as isentropic. Nozzle throat area must be ______ to sustain the flow. Air flows steadily through a converging-diverging nozzle a mass flow rate of3.00kg/s. The air enters the duct at a pressure of 1400kPa and a temperature of200°C with a low velocity, and it expands in the nozzle to an exit pressure of92kPa. The duct is designed so that the flow can be approximated as isentropic.Nozzle throat area must beto sustain the flow.Your answer

As given that In C-D nozzle mass flow rate (m)= 3 Kg/s ;P1= 1400kPa, T1= 200°C= 473 K, velocity is…

Answered: Air flows steadily through a…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Air flows steadily through a converging-diverging nozzle a mass flow rate of 3.00kg/s. The air enters the duct at a pressure of 1400kPa and a temperature of 200°C with a low velocity, and it expands in the nozzle to an exit pressure of 92kPa. The duct is designed so that the flow can be approximated as isentropic. Nozzle throat area must be ______ to sustain the flow.

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