Q.5 A supersonic wind tunnel, which is shown in the figure, is fed from a large tank. The air is discharged to the atmosphere. The Mach number in the test section is 2.65 and a normal shock wave stands at the exit of the wind tunnel. The pressure at section 3 immediately after the normal shock wave is 100 kPa. The flow is isentropic except through the normal shock wave. Find: 1. Po, P1, P2 and M3. 2. If a Pitot tube is placed in the exit jet, then calculate the pressure measured by the Pitot tube. 3. P. Test section Normal shock wave Exit Jet Pitot tube
Q.5 A supersonic wind tunnel, which is shown in the figure, is fed from a large tank. The air is discharged to the atmosphere. The Mach number in the test section is 2.65 and a normal shock wave stands at the exit of the wind tunnel. The pressure at section 3 immediately after the normal shock wave is 100 kPa. The flow is isentropic except through the normal shock wave. Find: 1. Po, P1, P2 and M3. 2. If a Pitot tube is placed in the exit jet, then calculate the pressure measured by the Pitot tube. 3. P. Test section Normal shock wave Exit Jet Pitot tube
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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Transcribed Image Text:Q.5 A supersonic wind tunnel, which is shown in the figure, is fed from a large tank.
The air is discharged to the atmosphere. The Mach number in the test section is 2.65
and a normal shock wave stands at the exit of the wind tunnel. The pressure at section
3 immediately after the normal shock wave is 100 kPa. The flow is isentropic except
through the normal shock wave. Find:
1. Po, P1, P2 and M3.
2. If a Pitot tube is placed in the exit jet, then calculate the pressure measured by the
Pitot tube.
Po
Test section
Normal shock wave
Exit Jet Pitot tube
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