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Carbon dioxide gas flows from a large tank (at temperature 50 °C and pressure 2 atmosphere under adiabatic conditions into a second tank through a horizontal converging nozzle) diameter of throat equal t7 cm) Z 40 The pressure at the second tank and at the nozzle throat is(1.3atmosphere. - Calculate the mass flow rate of carbon dioxide gas assuming frictionless flow. - Calculate Mach number in the nozzle throat. Molecular weight of Carbon dioxide = 44 C₂/C, (y) for Carbon dioxide = 1.3 Vie IRT Must

Carbon dioxide gas flows from a large tank (at temperature 50 °C and pressure 2 atmosphere under adiabatic conditions into a second tank through a horizontal converging nozzle) diameter of throat equal t7 cm) Z 40 The pressure at the second tank and at the nozzle throat is(1.3atmosphere. - Calculate the mass flow rate of carbon dioxide gas assuming frictionless flow. - Calculate Mach number in the nozzle throat. Molecular weight of Carbon dioxide = 44 C₂/C, (y) for Carbon dioxide = 1.3 Vie IRT Must

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
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O Carbon dioxide gas flows from a large tank (at temperature 50 °C and pressure 2 atmosphere) under adiabatic conditions into a second tank through a horizontal converging nozzle) diameter of throat equal t7 cm) of The pressure at the second tank and at the nozzle throat is 1.3atmosphere. 1- Calculate the mass flow rate of carbon dioxide gas assuming frictionless flow. 2- Calculate Mach number in the nozzle throat. IR T Molecular weight of Carbon dioxide = 44 C₂/C, (y) for Carbon dioxide = 1.3 H Vie Mut
Transcribed Image Text:O Carbon dioxide gas flows from a large tank (at temperature 50 °C and pressure 2 atmosphere) under adiabatic conditions into a second tank through a horizontal converging nozzle) diameter of throat equal t7 cm) of The pressure at the second tank and at the nozzle throat is 1.3atmosphere. 1- Calculate the mass flow rate of carbon dioxide gas assuming frictionless flow. 2- Calculate Mach number in the nozzle throat. IR T Molecular weight of Carbon dioxide = 44 C₂/C, (y) for Carbon dioxide = 1.3 H Vie Mut
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