(b) A normal shock wave passes through stagnant air at 22°C and atmospheric pressure of 130 kPa with a speed of 465 m/s as shown in Figure 3. Assume y= 1.4 and R= 287 J/kg.K. P, P2 V1 V2 Stationary shock wave
(b) A normal shock wave passes through stagnant air at 22°C and atmospheric pressure of 130 kPa with a speed of 465 m/s as shown in Figure 3. Assume y= 1.4 and R= 287 J/kg.K. P, P2 V1 V2 Stationary shock wave
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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Question
![(b) A normal shock wave passes through stagnant air at 22°C and atmospheric
pressure of 130 kPa with a speed of 465 m/s as shown in Figure 3. Assume
y= 1.4 and R= 287 J/kg.K.
P2
V1
V2
Stationary shock wave
Figure 3
[Gambarajah 3]
(i) Determine the pressure and temperature downstream of the normal shock
wave.
(ii) Determine the velocity in the air immediately behind the normal shock
wave.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F2b821139-cf08-406b-baa0-1f003c469379%2Fe0a0101f-ae53-48ab-aa50-40c07fffc8e2%2Fhablxbp_processed.jpeg&w=3840&q=75)
Transcribed Image Text:(b) A normal shock wave passes through stagnant air at 22°C and atmospheric
pressure of 130 kPa with a speed of 465 m/s as shown in Figure 3. Assume
y= 1.4 and R= 287 J/kg.K.
P2
V1
V2
Stationary shock wave
Figure 3
[Gambarajah 3]
(i) Determine the pressure and temperature downstream of the normal shock
wave.
(ii) Determine the velocity in the air immediately behind the normal shock
wave.
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