An ideal gas is to flow isentropically from a large tank where the air is maintained at a temperature and pressure of 59 °F and 114 psia to standard atmospheric discharge conditions in a way to achieve a maximal velocity. Describe in general terms the kind of duct involved and determine the duct exit Mach number and velocity in ft/s if the gas is air. The problem can be solved either using the isentropic relations or this figure. The isentropic relations are more accurate, but difficult to use unless you code them into a computer program. (a) What is the pressure ratio for the flow? (b) Is the exit flow subsonic, sonic, or supersonic? (c) What is the exit Mach number? (a) Pexit/PO 0.1289 (b) supersonic (c) Mexit 1.99 eTextbook and Media Hint Part 2 x Incorrect. The temperature needs to be in degrees absolute. (a) What is the exit temperature? (b) What is speed of sound at the exit? (c) What is the exit speed? (a) Texit" 320 (b) Cexit (c) Vexit 876.09 1747.33 R ft/s ft/s Assistance Used Attempts: 2 of 5 used

Elements Of Electromagnetics
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Correct. The pressure ratio is important to determining whether the flow is sonic or supersonic at the exit.
The exit Mach number is greater than unity and the flow at the exit is supersonic.
An ideal gas is to flow isentropically from a large tank where the air is maintained at a temperature and pressure of
59 °F and 114 psia to standard atmospheric discharge conditions in a way to achieve a maximal velocity. Describe
in general terms the kind of duct involved and determine the duct exit Mach number and velocity in ft/s if the gas is
air.
The problem can be solved either using the isentropic relations or this figure. The isentropic relations are more
accurate, but difficult to use unless you code them into a computer program.
(a) What is the pressure ratio for the flow?
(b) Is the exit flow subsonic, sonic, or supersonic?
(c) What is the exit Mach number?
(a) Pexit/PO
0.1289
(b) supersonic
(c) Mexit 1.99
eTextbook and Media
Hint
Part 2
=
* Incorrect. The temperature needs to be in degrees absolute.
(a) What is the exit temperature?
(b) What is speed of sound at the exit?
(c) What is the exit speed?
(a) Texit i 320
(b) Cexit
(c) Vexit i 1747.33
=
000
000
876.09
eTextbook and Media
Save for Later
R
ft/s
ft/s
MacBook Pro
*
8.
ㅎ
Assistance Used
Attempts: 2 of 5 used Submit Answer
DII
Attempts: 2 of 5 used
4
Transcribed Image Text:0 ✓ Correct. The pressure ratio is important to determining whether the flow is sonic or supersonic at the exit. The exit Mach number is greater than unity and the flow at the exit is supersonic. An ideal gas is to flow isentropically from a large tank where the air is maintained at a temperature and pressure of 59 °F and 114 psia to standard atmospheric discharge conditions in a way to achieve a maximal velocity. Describe in general terms the kind of duct involved and determine the duct exit Mach number and velocity in ft/s if the gas is air. The problem can be solved either using the isentropic relations or this figure. The isentropic relations are more accurate, but difficult to use unless you code them into a computer program. (a) What is the pressure ratio for the flow? (b) Is the exit flow subsonic, sonic, or supersonic? (c) What is the exit Mach number? (a) Pexit/PO 0.1289 (b) supersonic (c) Mexit 1.99 eTextbook and Media Hint Part 2 = * Incorrect. The temperature needs to be in degrees absolute. (a) What is the exit temperature? (b) What is speed of sound at the exit? (c) What is the exit speed? (a) Texit i 320 (b) Cexit (c) Vexit i 1747.33 = 000 000 876.09 eTextbook and Media Save for Later R ft/s ft/s MacBook Pro * 8. ㅎ Assistance Used Attempts: 2 of 5 used Submit Answer DII Attempts: 2 of 5 used 4
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