. An air tank with a nozzle has a pressure of 196.32 KPa and density of 1.9 Kg/m3. Outsic diverging nozzle, the pressure is atmospheric and designed to have a Mach No. of 1.0 an and exit respectively. The area at the throat is 0.11m?. Calculate the following: (a) Tempe of sound at the tank. (b) Pressure, density, temperature and speed of sound at the throa
. An air tank with a nozzle has a pressure of 196.32 KPa and density of 1.9 Kg/m3. Outsic diverging nozzle, the pressure is atmospheric and designed to have a Mach No. of 1.0 an and exit respectively. The area at the throat is 0.11m?. Calculate the following: (a) Tempe of sound at the tank. (b) Pressure, density, temperature and speed of sound at the throa
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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![2. An air tank with a nozzle has a pressure of 196.32 KPa and density of 1.9 Kg/m³. Outside the converging-
diverging nozzle, the pressure is atmospheric and designed to have a Mach No. of 1.0 and 1.5 at the throat
and exit respectively. The area at the throat is 0.11m2. Calculate the following: (a) Temperature and speed
of sound at the tank. (b) Pressure, density, temperature and speed of sound at the throat. (c) Mass flow at
the exit.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F061d3272-0af8-45de-8848-27f401374c63%2Ff330d39d-dad3-49a2-8aec-be404930d871%2F1kfzpar_processed.jpeg&w=3840&q=75)
Transcribed Image Text:2. An air tank with a nozzle has a pressure of 196.32 KPa and density of 1.9 Kg/m³. Outside the converging-
diverging nozzle, the pressure is atmospheric and designed to have a Mach No. of 1.0 and 1.5 at the throat
and exit respectively. The area at the throat is 0.11m2. Calculate the following: (a) Temperature and speed
of sound at the tank. (b) Pressure, density, temperature and speed of sound at the throat. (c) Mass flow at
the exit.
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