Required information Problem 05.042 Nozzle flow Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area of the nozzle is 110 cm². The gas constant of air is 0. 287 kPa m³/kg K. The specific heat of air at the anticipated average temperature of 450 K is Cp 1.02 kJ/kg. C. . P₁ = 300 kPa T₁ =200°C Air P₂ kPa V₁ -45 m/s V₂ = 180 m/s A₁ = 110 cm² Problem 05.042.a- Nozzle flow Determine the mass flow rate through the nozzle. The mass flow rate through the nozzle is kg/s. 0 Required information Problem 05.042 Nozzle flow Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area of the nozzle is 110 cm2. The gas constant of air is 0.287 kPa m³/kg K. The specific heat of air at the anticipated average temperature of 450 K is cp = 1.02 kJ/kg. C. - P₁ = 300 kPa T₁ =200°C V₁=45 m/s A₁ = 110 cm² Air P2 kPa V2 180 m/s Problem 05.042.b - Nozzle flow Determine the exit temperature of the air. The exit temperature of the air is °C.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Required information
Problem 05.042 Nozzle flow
Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area
of the nozzle is 110 cm². The gas constant of air is 0. 287 kPa m³/kg K. The specific heat of air at the anticipated
average temperature of 450 K is Cp 1.02 kJ/kg. C.
.
P₁ = 300 kPa
T₁ =200°C
Air
P₂ kPa
V₁
-45 m/s
V₂ = 180 m/s
A₁ = 110 cm²
Problem 05.042.a- Nozzle flow
Determine the mass flow rate through the nozzle.
The mass flow rate through the nozzle is
kg/s.
Transcribed Image Text:Required information Problem 05.042 Nozzle flow Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area of the nozzle is 110 cm². The gas constant of air is 0. 287 kPa m³/kg K. The specific heat of air at the anticipated average temperature of 450 K is Cp 1.02 kJ/kg. C. . P₁ = 300 kPa T₁ =200°C Air P₂ kPa V₁ -45 m/s V₂ = 180 m/s A₁ = 110 cm² Problem 05.042.a- Nozzle flow Determine the mass flow rate through the nozzle. The mass flow rate through the nozzle is kg/s.
0
Required information
Problem 05.042 Nozzle flow
Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area
of the nozzle is 110 cm2. The gas constant of air is 0.287 kPa m³/kg K. The specific heat of air at the anticipated
average temperature of 450 K is cp = 1.02 kJ/kg. C.
-
P₁ = 300 kPa
T₁ =200°C
V₁=45 m/s
A₁ = 110 cm²
Air
P2 kPa
V2 180 m/s
Problem 05.042.b - Nozzle flow
Determine the exit temperature of the air.
The exit temperature of the air is
°C.
Transcribed Image Text:0 Required information Problem 05.042 Nozzle flow Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 110.0 kPa and 180 m/s. The inlet area of the nozzle is 110 cm2. The gas constant of air is 0.287 kPa m³/kg K. The specific heat of air at the anticipated average temperature of 450 K is cp = 1.02 kJ/kg. C. - P₁ = 300 kPa T₁ =200°C V₁=45 m/s A₁ = 110 cm² Air P2 kPa V2 180 m/s Problem 05.042.b - Nozzle flow Determine the exit temperature of the air. The exit temperature of the air is °C.
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