FUND OF ENG THERMODYN(LLF)+WILEYPLUS
9th Edition
ISBN: 9781119391777
Author: MORAN
Publisher: WILEY
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Air as an ideal gas flows through the compressor and heat exchanger shown in the figure. A separate liquid stream also flows through the heat exchanger. The data given are for operation at steady state. Stray heat transfer to the surroundings can be neglected, as can all kinetic and potential energy changes. Determine the compressor power, in kW, and the mass flow rate of the cooling water, in kg/s.
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A pump is used to circulate hot water in a home heating system. Water enters the well-insulated pump operating at steady state at a
rate of 0.42 gal/min. The inlet pressure and temperature are 14.7 lbf/in.², and 180°F, respectively; at the exit the pressure is 90 lbf/in.²
The pump requires 1/15 hp of power input. Water can be modeled as an incompressible substance with constant density of 60.58
lb/ft3 and constant specific heat of 1 Btu/lb. °R.
Neglecting kinetic and potential energy effects, determine the temperature change, in °R, as the water flows through the pump.
ΔΤ :
= i 0.36
°R
Steam at 44 bar and a dryness fraction, x = 0.9 is throttled to a pressure of 12 bar. Calculate thedifference in power output in kilowatts between the following two expansion processes:a) Steam at the initial pressure of 44 bar and x = 0.9 at State 1 is expanded in a turbine to State 3 at 0.12 bar.b) Steam at the reduced pressure of 12 bar after throttling at State 2 is expanded in another turbine to State 4 at the same exhaust pressure of 0.12 bar.The mass flow rate of steam is 8 kg/sec in both cases and the expansion in both turbines can be assumed to be reversible and adiabatic. Sketch both expansion processes on the same T-s diagram using the respective initial and final state points as described above.Explain the reason for the difference in power output.Calculate the mass flow rate of steam for the turbine operating at the throttled/reduced pressure to generate the same output as the turbine operating at the pressure before throttling.NOTE: You are required to number the state…
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- Item 9 An open system with only one inlet and one exit operates at steady state. Mass enters the system at a flow rate of 8 kg/s with the following properties: h = 3245 kJ/kg, s = 8.0514 kJ/kg - K, and V = 18 m/s. At the exit the properties are as follows: h = 2139 kJ/kg, s = 8.089 kJ/kg · K, and V = 29 m/s. The device produces 8799 kW shaft work while rejecting some heat to the atmosphere at 30 °C. Part A Do a mass analysis to determine the mass flow rate at the exit. Express your answer to three significant figures. ΑΣφ |vec ? Submit Request Answer Part B Do an energy analysis to determine the rate of heat transfer (include sign). Express your answer to three significant figures and include the appropriate units. ? Value Units Submit Request Answer Part C Do an entropy analysis to evaluate the rate of entropy generation in the system's universe. Express your answer to three significant figures. ΑΣφ vec ? kW Karrow_forwardA turbine, operating under steady-flow conditions, receives X1 kg of steam per hour (For X1 refer Table. 1). The steam enters the turbine at a velocity of 3000 m/min, an elevation of 5 m and a specific enthalpy of 2787 kJ/kg. It leaves the turbine at a velocity of 6000 m/min, an elevation of 1 m and a specific enthalpy of 2259 kJ/kg. Heat losses from the turbine to the surroundings amount to 16736 kJ/h. Determine the power output of the turbine.arrow_forward6.111 Steam enters a two-stage turbine with reheat operating at steady state as shown in Fig. P6.111. The steam enters turbine 1 with a mass flow rate of 120,000 lb/h at 1000 lbf/in.², 800°F and expands to a pressure of 60 lbf/in. From there, the steam enters the reheater where it is heated at constant pressure to 350°C before entering tur- bine 2 and expanding to a final pressure of 1 lbf/in.? The turbines operate adiabatically with isentropic efficiencies of 88% and 85%, respectively. Kinetic and potential energy effects can be neglected. Determine the net power developed by the two turbines and the rate of heat transfer in the reheater, each in Btu/h. Qin P3 = 60 lbf/in.2 T = 350°C P2 = 60 lbf/in.2 Reheater W net Turbine 1 Turbine 2 Nu = 88% Ni2 = 85% P4 =1 lbf/in.2 P1 = 1000 Ibf/in.2 T = 800°F m = 120,000 lb/h FIGURE P6.111arrow_forward
- Determine:(a) the total power for both compressors, in kW.(b) the mass flow rate of the water, in kg/s.arrow_forwardCurrent Attempt in Progress A pump is used to circulate hot water in a home heating system. Water enters the well-insulated pump operating at steady state at a rate of 0.42 gal/min. The inlet pressure and temperature are 14.7 Ibf/in.?, and 180°F, respectively; at the exit the pressure is 90 Ibf/in.2 The pump requires 1/25 hp of power input. Water can be modeled as an incompressible substance with constant density of 60.58 Ib/ft and constant specific heat of 1 Btu/lb · °R. Neglecting kinetic and potential energy effects, determine the temperature change, in °R, as the water flows through the pump. AT = i °Rarrow_forwarduse table Table Derive expressions for the heat absorbed by the system for each of the following classes of reversible processes for one mole of an idea gas: (a) Case 1: Isothermal change in pressure (b) Case 2: Isobaric change in volume Hint: Case 1 with S = S(T,P); Case 2 with S = S(P,V) (c) Case 3: Isochoric (constant volume) change in temperature dV=Va dT-VB AP dS=CT dT-Va dP dU= (Cp-PVα) dT + V(PB - Ta) dP dH=Cp dT +V(I-Ta) dP dF=-(S+PVa) dT + VPB dP dG=-S dT + V dParrow_forward
- Problem #1: Helium gas flows through a well-insulated nozzle at steady state. The temperature and velocity at the inlet are 550 °R and 150 ft/s, respectively. At the exit, the temperature is 400 °R and the pressure is 40 psi. The area of the exit is 0.0085 ft². Using the ideal gas model with k=1.67, and neglecting potential energy effects, determine the mass flow rate, in lbm/s through the nozzle.arrow_forwardT-7arrow_forwardRefrigerant 134a enters an insulated diffuser as a saturated vapor at 120°F with a velocity of 1400 ft/s. The inlet area is 1.4 in?. At the exit, the pressure is 400 Ibf/in2 and the velocity is negligible. The diffuser operates at steady state and potential energy effects can be neglected. Determine the mass flow rate, in Ib/s, and the exit temperature, in °F.arrow_forward
- 4. Considering the Typical Energy Balance for gasoline engine, @ atmospheric condition of 1.013 bar and 26°C with constant speed of 2800 rpm, intake air flow rate of 190 Kg/hr, and volumetric efficiency of 75%. If 16.61 KW of energy loss to surrounding was considered. Determine a. The amount of torque in Nm needed b. The mass flow rate of fuel in Kg/hr with calorific value of 45 400 KJ/Kg c. The volume displacement Note: Typical Full Load Energy Balance for Gasoline Engine based on 100% fuel input ЕСТВР -25% ELTCW -30% ELTEG - 37% ELTS 8%arrow_forwardA power washer is being used to clean the siding of a house. Water enters at 20 ◦C (specific volume = 1.0018×10−3 m3/kg), 1 atm, with a volumetric flow rate of 0.1 L/s through a 2.5 cm diameter hose. A jet water exits at 23 ◦C, 1 atm, with a velocity of 50 m/s at an elevation of 10 m. At steady state, the magnitude of the heat transfer rate from the power unit to the surroundings is 10% of the power input. The water can be considered incompressible with specific heat equal to 4.18 kJ/kg · K and g = 9.81 m/s2. What is the power input to the motor in kW?arrow_forward6.107 Figure P6.107 provides the schematic of a heat pump using Refrigerant 134a as the working fluid, together with steady-state data at key points. The mass flow rate of the refrigerant is 7 kg/min, and the power input to the compressor is 5.17 kW. (a) Determine the co- efficient of performance for the heat pump. (b) If the valve were re- placed by a turbine, power could be produced, thereby reducing the power requirement of the heat pump system. Would you recommend this power-saving measure? Explain. She P2 = P3 = 9 bar Tz = 60°C Saturated liquid Condenser Expansion W = 5.17 kW Compressor valve Evaporator m= 7 kg/min P1 =P4 = 2.4 bar FIGURE P6.107arrow_forward
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