Example 5 An airstream with Mach number of 2, a pressure of 150 KPa and a temperature of 350K enters a diverging channel as shown in the figure. If the ratio of the exit cross-sectional are to the inlet cross-sectional are 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 isentropic flow except through the normal shock wave. Ans. 444.2 KPa P = 150KPA T= 350K M = 2 A1 = A2 = 2A; A= 3A; 1 2
Example 5 An airstream with Mach number of 2, a pressure of 150 KPa and a temperature of 350K enters a diverging channel as shown in the figure. If the ratio of the exit cross-sectional are to the inlet cross-sectional are 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 isentropic flow except through the normal shock wave. Ans. 444.2 KPa P = 150KPA T= 350K M = 2 A1 = A2 = 2A; A= 3A; 1 2
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
Related questions
Question
I need the answer quickly

Transcribed Image Text:Example 5
An airstream with Mach number of 2, a pressure of
150 KPa and a temperature of 350K enters a diverging
channel as shown in the figure. If the ratio of the exit
cross-sectional are to the inlet cross-sectional are 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 isentropic flow except
through the normal shock wave.
Ans. 444.2 KPa
A1 = A2 = 2A;
P= 150KPA
T = 350K
Mi = 2
A= 3A;
(1)
Expert Solution

This question has been solved!
Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.
This is a popular solution!
Trending now
This is a popular solution!
Step by step
Solved in 2 steps with 2 images

Recommended textbooks for you

Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press

Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON

Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education

Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press

Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON

Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education

Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY

Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning

Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY