For a nozzle-duct system shown in Fig.Q3, the nozzle is designed to produce a Mach number of 2.8 with y = 1.4. The inlet conditions are p01 = 10 bar and To1 370 K. The duct is 8 diameters in length, but the duct friction factor is unknown. The receiver pressure is fixed at 3 bar and a normal shock has formed at the duct exit. (a) Determine the friction factor of the duct. (b) What is the total change in entropy for the system? - 10 bar T- 370 K Pre 3 bar f-? Fig.Q3 -Ax $D

Elements Of Electromagnetics
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Q3/
For a nozzle-duct system shown in Fig.Q3, the nozzle is designed to produce a Mach number of
2.8 with y = 1.4. The inlet conditions are po1 = 10 bar and To1 = 370 K. The duct is 8 diameters in
length, but the duct friction factor is unknown. The receiver pressure is fixed at 3 bar and a
normal shock has formed at the duct exit.
(a) Determine the friction factor of the duct.
(b) What is the total change in entropy for the system?
= 10 bar
T- 370 K
Pre=3 bar
f-?
Fig.Q3
Ax $D
Q4/
Transcribed Image Text:Q3/ For a nozzle-duct system shown in Fig.Q3, the nozzle is designed to produce a Mach number of 2.8 with y = 1.4. The inlet conditions are po1 = 10 bar and To1 = 370 K. The duct is 8 diameters in length, but the duct friction factor is unknown. The receiver pressure is fixed at 3 bar and a normal shock has formed at the duct exit. (a) Determine the friction factor of the duct. (b) What is the total change in entropy for the system? = 10 bar T- 370 K Pre=3 bar f-? Fig.Q3 Ax $D Q4/
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