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Air flows through a converging-diverging (c-d) nozzle. It is supplied from a large air reservoir in which the temperature is 446 K and the pressure is 190 kPa. The velocity and the cross- sectional area at the nozzle exit are 594 m/s and 0.0005 m^2, respectively. Find the elp me solve this problem :followings of dynamic gases

Air flows through a converging-diverging (c-d) nozzle. It is supplied from a large air reservoir in which the temperature is 446 K and the pressure is 190 kPa. The velocity and the cross- sectional area at the nozzle exit are 594 m/s and 0.0005 m^2, respectively. Find the elp me solve this problem :followings of dynamic gases

Elements Of Electromagnetics
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 through a converging-diverging (c-d) nozzle. It is supplied from a large air reservoir in which the temperature is 446 K and the pressure is 190 kPa. The velocity and the cross- sectional area at the nozzle exit are 594 m/s and 0.0005 m^2, respectively. Find the Help me solve this problem :followings of dynamic gases
Transcribed Image Text:Air flows through a converging-diverging (c-d) nozzle. It is supplied from a large air reservoir in which the temperature is 446 K and the pressure is 190 kPa. The velocity and the cross- sectional area at the nozzle exit are 594 m/s and 0.0005 m^2, respectively. Find the Help me solve this problem :followings of dynamic gases
Mach number at exit is 1.2 O 1.8 1.6 O 1.4 1.1 1.3 O Area of the throat is 1.48 E-4 m^2 O 4 E-4 m^2 O 2.45 E-4 m^2 O 4.485 E-4 m^2 4.85 E-4 m^2 O 3.475 E-4 m^2 O The mass flow rate of air is 0.215 kg/s O 0.178 kg/s 0.152 kg/s O 0.101 kg/s O 0.127 kg/s O 0.199 kg/s O The exit temperature is 241 K O 210 K O 251 K O 285 K 221 K O 271 к О The exit pressure is 78.4 kPa O 33.1 КРа О 55.7 КРа О 85.6 kPa 44.7 kPa O 22.5 kPa ООО О оо O o O O O o o o O o O O O O C
Transcribed Image Text:Mach number at exit is 1.2 O 1.8 1.6 O 1.4 1.1 1.3 O Area of the throat is 1.48 E-4 m^2 O 4 E-4 m^2 O 2.45 E-4 m^2 O 4.485 E-4 m^2 4.85 E-4 m^2 O 3.475 E-4 m^2 O The mass flow rate of air is 0.215 kg/s O 0.178 kg/s 0.152 kg/s O 0.101 kg/s O 0.127 kg/s O 0.199 kg/s O The exit temperature is 241 K O 210 K O 251 K O 285 K 221 K O 271 к О The exit pressure is 78.4 kPa O 33.1 КРа О 55.7 КРа О 85.6 kPa 44.7 kPa O 22.5 kPa ООО О оо O o O O O o o o O o O O O O C
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