5-36 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 110 cm². Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle.
5-36 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 110 cm². Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle.
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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![5-36 Air enters an adiabatic nozzle steadily at 300 kPa,
200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The
inlet area of the nozzle is 110 cm². Determine (a) the mass
flow rate through the nozzle, (b) the exit temperature of the air,
and (c) the exit area of the nozzle.
P₁ = 300 kPa
T₁ = 200°C
V₁ = 45 m/s
A₁ = 110 cm²
FIGURE P5-36
Air
P2 = 100 kPa
V₂ = 180 m/s](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F36361dfa-b5ec-4d30-a81f-90380d20c66d%2F2f6cb785-23f7-4a43-83cb-06fc51278904%2F9zlsgrh_processed.jpeg&w=3840&q=75)
Transcribed Image Text:5-36 Air enters an adiabatic nozzle steadily at 300 kPa,
200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The
inlet area of the nozzle is 110 cm². Determine (a) the mass
flow rate through the nozzle, (b) the exit temperature of the air,
and (c) the exit area of the nozzle.
P₁ = 300 kPa
T₁ = 200°C
V₁ = 45 m/s
A₁ = 110 cm²
FIGURE P5-36
Air
P2 = 100 kPa
V₂ = 180 m/s
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