FUNDAMENTALS OF THERMODYNAMICS
10th Edition
ISBN: 9781119634928
Author: Borgnakke
Publisher: WILEY
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A certain SSSF turbine (irreversible and adiabatic) operates on air with the following conditions,
Inflow: Ti=1000 K, Pi = 13223.07354 kPa
Outflow (actual): Te = 402.3904382 K
Find the actual specific work output of the turbine, wt in KJ/kg.
(Assume single inflow/outflow, neglect change in KE and PE. Assume constant specific heats in this
problem, with Cp0 =1.004 kJ/(K*kg) and k= 1.4.
Next if the hypothetical ideal, reversible adiabatic (isentropic) specific work output of the turbine is wt=
+800 Kj/kg:
Find the isentropic efficiency of the turbine, outflow pressure Pe in kPa and finally what is the ratio of
the outflow pressure of the actual turbine to the same pressure for the ideal turbine.
2. If 0.17 kg/s of air are compressed isothermally from Pi = 96 kPaa and V, = 0.13
m/s to p2 = 620 kPaa, find the work, the change of entropy, and heat for: a) a
nonflow process, and b) a steady flow process with V1 = 15 m/s and V2 = 60
%3D
%3D
m/s.
5.49 Air in a piston/cylinder goes through a
Carnot cycle with the P-v diagram shown
in Fig. 5.21. The high and low temperatures
are 600 K and 300 K, respectively. The heat
added at the high temperature is 250 kJ/kg,
and the lowest pressure in the cycle is 75
kPa. Find the specific volume and pressure
after heat rejection and the net work per
unit mass.
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- Velocity ratio of a machine is 72. The law of machine is P=1/48 W+30 N. Find the maximum MA, efficiency and state whether machine is reversible. KINDLY SOLVE THIS...please.arrow_forwardSteam enters a continuous flow turbine at a pressure of 8 MPa and a temperature of 450 ℃ and reaches a pressure of 70 kPa it is expanding. The mass flow rate of the steam is 200000 kg/hour and it is in the form of saturated steam at the outlet. By accepting the ambient temperature, 25℃ and pressure 100 kPa; a) The power potential of the steam at the inlet conditions b) Can you find the turbine power output for the situation where there are no irreversibilities? (Kinetic and potential energy ignore the changes).arrow_forward2. A two-stage air compressor has an intercooler between the two stages as shown below. The inlet state is 100 kPa, 290 K, and the final exit pressure is 1.6 MPa. Assume that the constant pressure intercooler cools the air to the inlet temperature, T= T1. It can be shown that the optimal pressure, P,= (P.Pa for minimum total compressor work. Find the specific compressor works, the intercooler heat transfer for the optimal P, and sketch and label the P-v and T-s diagrams. otf Corpressor Compressor Intercoolerarrow_forward
- 20. If 10 kg/min of air are compressed isothermally from P1 = 96 kPa and Vi 7.65 m³/min to P2 = 620 kPa, find the work, change in entropy %3D for a non-flow process and a steady flow process with vị = 15 m/s and v2 = 60 m/s.arrow_forwardA stationary diesel engine with a thermal efficiency of 40% produces 200 horsepower. The exhaust gas, which we suppose is air, has a velocity of 1400 R, whereas the intake has a velocity of 520 R. What is the mass flow rate if it accounts for half of the QL?arrow_forwardA: Derive the steady flow energy equation and reduce it for a. A turbine (Reversible Process) b. A pump (Reversible Process) c. A nozzle (Reversible Process) d. A throttling (Irreversible Process)arrow_forward
- A turbine, operating under steady- flow conditions, reccives 1000 kg/min of stcam. At the inlet, the pressure is 30 bar, the temperature is 400°C, the velocity At the exit, the pressure is 0.7 bar, the quality is (100%), and the velocity is 100 m/s. If the turbine produced a power output of 9300 KW. By using the energy balance of open system with sutable tables, answer the following: (a) What are the main assumptions ? (b) Calculate dh, AKe ? (c) Calculate the rate of heat transfer between the turbine and surroundings, in kW.arrow_forward4. A compressor draws in 500 min ft³ of air whose density is 0.079 lb and discharges lb At the suction, P, = 15 - lb it with a density of 0.304 and at the discharge, in? lb The increase in the specific internal energy is 33.8 Btu and the lb P2 = 80 in? Btu heat from the air by cooling is 13. Neglecting changes in the potential and lb Btu kinetic energy determine the work done on the air in min and in horsepower.arrow_forwardAn internally reversible process occurs in a system during which Q = – 12 KJ, AU = – 79 KJ and Ah = - 111 KJ A. Find the work if the system is non- flow. B. Determine the work and the change of flow energy if the system is steady state, steady flow system with AEK 4 KJ. %3Darrow_forward
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