ir enters an adiabatic nozzle steadily at 345 kPa, 207 oC, and 73 m/s and leaves at 199 kPa and 185 m/s. The inlet area of the nozzle is 135 cm2. Determine: (a) the mass flow rate through the nozzle (kg/s), (b) the exit temperature of the air (oC), and (c) the exit area of the nozzle (cm2). Submit your solution by multiplying (a)*(b)*(c) = _______. (Use T = 450 K to get the value of cp).
ir enters an adiabatic nozzle steadily at 345 kPa, 207 oC, and 73 m/s and leaves at 199 kPa and 185 m/s. The inlet area of the nozzle is 135 cm2. Determine: (a) the mass flow rate through the nozzle (kg/s), (b) the exit temperature of the air (oC), and (c) the exit area of the nozzle (cm2). Submit your solution by multiplying (a)*(b)*(c) = _______. (Use T = 450 K to get the value of cp).
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 enters an adiabatic nozzle steadily at 345 kPa, 207 oC, and 73 m/s and leaves at 199 kPa and 185 m/s. The inlet area of the nozzle is 135 cm2. Determine: (a) the mass flow rate through the nozzle (kg/s), (b) the exit temperature of the air (oC), and (c) the exit area of the nozzle (cm2). Submit your solution by multiplying (a)*(b)*(c) = _______.
(Use T = 450 K to get the value of cp).
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