2. (40) A turbojet operates with the conditions listed below, with an ideal gas with
constant specific heats; cp=1004 J/(kg K) and k=1.4. Use the air standard model. Use
the state numbering system shown in Example 9.13 of the text. Processes a-1-2 and
3-4-5 are adiabatic. All processes except the compressor in part b are internally
reversible. The devices operate at steady state. Neglect potential energy effects. It
is not necessary to verify the validity of the properties listed in the table:
STATE
T, K
p, bar
Velocity, m/s
a (diffuser inlet)
240
0.35
200
1 (compressor inlet)
260.0
0.463
approx. 0
2 (combustor inlet)
T2
4.63
approx. 0
3 (turbine inlet)
1400
4.63
approx. 0
4 (nozzle inlet)
T4
P4
approx. 0
5 (nozzle exit)
T5
0.35
V5
a) Find T2, T4, p4, T5, and V5 if the compressor is internally reversible.
b) Find T2, T4, p4, T5, and V5 if the compressor has an isentropic efficiency of 75%