As shown in Figure 1, an ideal gas flows isentropically from a large tank into a converging ozzle and exits to a receiver. The gauge pressure of the ideal gas in the large tank is 80 kPa. The nozzle exit area is 38 cm?. (Assume Pam = 101 kPa). a) Determine Mach Number at section 1, the EXIT mass flow rate and EXIT Mach number. b) Calculate the flow area at section 1. V:= 580 kan hr T;= 500 K Exit, A. Large Tank P= 166 kPa (abs) Ideal Gas k=1.43 R=0.2968 kJhg.k

Engineering Fundamentals: An Introduction to Engineering (MindTap Course List)
5th Edition
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Author:Saeed Moaveni
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Chapter10: Force And Force-related Variables In Engineering
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As shown in Figure 1, an ideal gas flows isentropically from a large tank into a converging
nozzle and exits to a receiver. The gauge pressure of the ideal gas in the large tank is 80 kPa.
The nozzle exit area is 38 cm?. (Assume Pam = 101 kPa).
a) Determine Mach Number at section 1, the EXIT mass flow rate and EXIT Mach mumber.
b) Calculate the flow area at section 1.
V: = 580 km/hr
T:= 500 K
Exit, A
Large Tank
P= 166 kPa (abs)
Ideal Gas
k=1.43
R= 0.2968 kJ/kg.k
Vi = 480 kan/hr
Figure 1
Transcribed Image Text:As shown in Figure 1, an ideal gas flows isentropically from a large tank into a converging nozzle and exits to a receiver. The gauge pressure of the ideal gas in the large tank is 80 kPa. The nozzle exit area is 38 cm?. (Assume Pam = 101 kPa). a) Determine Mach Number at section 1, the EXIT mass flow rate and EXIT Mach mumber. b) Calculate the flow area at section 1. V: = 580 km/hr T:= 500 K Exit, A Large Tank P= 166 kPa (abs) Ideal Gas k=1.43 R= 0.2968 kJ/kg.k Vi = 480 kan/hr Figure 1
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