3. A converging nozzle is fed with air from a large reservoir where the temperature and pressure are 400 K and 170 kPa, respectively. The nozzle has an exit cross-sectional area of 0.001 m? and discharges into the atmosphere with a pressure of 100 kPa. The flow is isentropic throughout the nozzle. Determine the pressure, Mach number, temperature and velocity at the exit plane, and also find the mass flow rate. (Ans: 100 kPa, 0.9, 344.8 K, 334.8 m-s, 0.3388 kg-s").

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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3. A converging nozzle is fed with air from a
large reservoir where the temperature and
pressure are 400 K and 170 kPa, respectively.
The nozzle has an exit cross-sectional area of
0.001 m? and discharges into the atmosphere
with a pressure of 100 kPa. The flow is
isentropic throughout the nozzle. Determine
the pressure, Mach number, temperature and
velocity at the exit plane, and also find the
mass flow rate. (Ans: 100 kPa, 0.9, 344.8 K,
334.8 m-s, 0.3388 kg-s).
Transcribed Image Text:3. A converging nozzle is fed with air from a large reservoir where the temperature and pressure are 400 K and 170 kPa, respectively. The nozzle has an exit cross-sectional area of 0.001 m? and discharges into the atmosphere with a pressure of 100 kPa. The flow is isentropic throughout the nozzle. Determine the pressure, Mach number, temperature and velocity at the exit plane, and also find the mass flow rate. (Ans: 100 kPa, 0.9, 344.8 K, 334.8 m-s, 0.3388 kg-s).
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