Q.1 An airstream with Mach number of 2, a pressure of 150 kPa and a temperature of 350 K enters a diverging channel as shown in the figure. If the ratio of the exit cross-sectional area to the inlet cross-sectional area is 3, determine the back pressure which is necessary to produce a normal shock wave in the channel with a cross- sectional area equal to twice the inlet cross-sectional area. Assume steady, one- dimensional and isentropic flow except through the normal shock wave. P = 150KPA T; = 350K M = 2 A1 = A2 = 2A; A. = 3A; %3!
Q.1 An airstream with Mach number of 2, a pressure of 150 kPa and a temperature of 350 K enters a diverging channel as shown in the figure. If the ratio of the exit cross-sectional area to the inlet cross-sectional area is 3, determine the back pressure which is necessary to produce a normal shock wave in the channel with a cross- sectional area equal to twice the inlet cross-sectional area. Assume steady, one- dimensional and isentropic flow except through the normal shock wave. P = 150KPA T; = 350K M = 2 A1 = A2 = 2A; A. = 3A; %3!
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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![Q.1 An airstream with Mach number of 2, a pressure of 150 kPa and a temperature
of 350 K enters a diverging channel as shown in the figure. If the ratio of the exit
cross-sectional area to the inlet cross-sectional area is 3, determine the back pressure
which is necessary to produce a normal shock wave in the channel with a cross-
sectional area equal to twice the inlet cross-sectional area. Assume steady, one-
dimensional and isentropic flow except through the normal shock wave.
P; = 150KPA
T; = 350K
M = 2
A1 = A2 = 2A;
A= 3A;
(2)](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fbf2a88fd-1768-4ee2-81db-ebec0afac10b%2Fa2b5bcb1-87ab-4948-9681-4edd2c2c8357%2F7oq525_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Q.1 An airstream with Mach number of 2, a pressure of 150 kPa and a temperature
of 350 K enters a diverging channel as shown in the figure. If the ratio of the exit
cross-sectional area to the inlet cross-sectional area is 3, determine the back pressure
which is necessary to produce a normal shock wave in the channel with a cross-
sectional area equal to twice the inlet cross-sectional area. Assume steady, one-
dimensional and isentropic flow except through the normal shock wave.
P; = 150KPA
T; = 350K
M = 2
A1 = A2 = 2A;
A= 3A;
(2)
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