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Methane is flowing through a well insulated converging-diverging nozzle. At the inlet, the pressure of methane is 161 bar, its temperature is -44.43 °C and its velocity is 20 m/sec. At the exit, the corresponding values for pressure and temperature of methane are 115 bar and -157.79 °C. Calculate the velocity of methane at the exit of the nozzle as well as the ratio of the cross sectional areas of the nozzle.

Methane is flowing through a well insulated converging-diverging nozzle. At the inlet, the pressure of methane is 161 bar, its temperature is -44.43 °C and its velocity is 20 m/sec. At the exit, the corresponding values for pressure and temperature of methane are 115 bar and -157.79 °C. Calculate the velocity of methane at the exit of the nozzle as well as the ratio of the cross sectional areas of the nozzle.

Introduction to Chemical Engineering Thermodynamics
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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Methane is flowing through a well insulated converging-diverging nozzle. At the inlet, the pressure of methane is 161 bar, its temperature is -44.43 °C and its velocity is 20 m/sec. At the exit, the corresponding values for pressure and temperature of methane are 115 bar and -157.79 °C. Calculate the velocity of methane at the exit of the nozzle as well as the ratio of the cross sectional areas of the nozzle.
Transcribed Image Text:Methane is flowing through a well insulated converging-diverging nozzle. At the inlet, the pressure of methane is 161 bar, its temperature is -44.43 °C and its velocity is 20 m/sec. At the exit, the corresponding values for pressure and temperature of methane are 115 bar and -157.79 °C. Calculate the velocity of methane at the exit of the nozzle as well as the ratio of the cross sectional areas of the nozzle.
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