Please do it correctly and step by step. 4. A converging-diverging nozzle is designed for Mach Number, M = 2.0 at the exit. Air is supplied at 900 kPa and500 K. Use Table A-32, and k-1.4 with R=0.287 kJ/kgK. You're asked by the division Vice President at yourplace of employment (oddly enough, even though you don't work in aerospace) to figure out the exit speed ofthe air to resolve some noise abatement complaints by neighbors at the local airport.a) To show you know the concept of converging-diverging nozzles, what is the throat temperature (K)?b) What is the throat velocity (m/s)?c) Now calculate the exit parameters, starting with the exit pressure (kPa). What is the exit pressure?d) What is the exit temperature (K)?e) Finally, what is the exit speed (m/s)?

Given mech number at exit (me) = 2 Given pressure (P1)=900kpa Given temperature (T1)=500 k

4. A converging-diverging nozzle is designed for Mach Number, M = 2.0 at the exit. Air is supplied at 900 500 K. Use Table A-32, and k-1.4 with R=0.287 kJ/kgK. You're asked by the division Vice President a place of employment (oddly enough, even though you don't work in aerospace) to figure out the exit s the air to resolve some noise abatement complaints by neighbors at the local airport. To show you know the concept of converging-diverging nozzles, what is the throat temperature (K)? What is the throat velocity (m/s)? Now calculate the exit parameters, starting with the exit pressure (kPa). What is the exit pressure? What is the exit temperature (K)? Finally, what is the exit speed (m/s)?

4. A converging-diverging nozzle is designed for Mach Number, M = 2.0 at the exit. Air is supplied at 900 500 K. Use Table A-32, and k-1.4 with R=0.287 kJ/kgK. You're asked by the division Vice President a place of employment (oddly enough, even though you don't work in aerospace) to figure out the exit s the air to resolve some noise abatement complaints by neighbors at the local airport. To show you know the concept of converging-diverging nozzles, what is the throat temperature (K)? What is the throat velocity (m/s)? Now calculate the exit parameters, starting with the exit pressure (kPa). What is the exit pressure? What is the exit temperature (K)? Finally, what is the exit speed (m/s)?

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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Concept explainers

Basic Terminology in Mechanics

The area of science and mathematics concerned the motion of the objects, the relation between the force matter, and motion if specified. Forces exerted over the objects result in displacements or changes in the position of an object concerning its environment. This branch of physics keeps its roots in Ancient Greece in the form of the scripts of Aristotle and Archimedes.

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Please do it correctly and step by step.

4. A converging-diverging nozzle is designed for Mach Number, M = 2.0 at the exit. Air is supplied at 900 kPa and
500 K. Use Table A-32, and k-1.4 with R=0.287 kJ/kgK. You're asked by the division Vice President at your
place of employment (oddly enough, even though you don't work in aerospace) to figure out the exit speed of
the air to resolve some noise abatement complaints by neighbors at the local airport.
a) To show you know the concept of converging-diverging nozzles, what is the throat temperature (K)?
b) What is the throat velocity (m/s)?
c) Now calculate the exit parameters, starting with the exit pressure (kPa). What is the exit pressure?
d) What is the exit temperature (K)?
e) Finally, what is the exit speed (m/s)?

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