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Concept explainers
- (a) Water flows through a shower head steadily at a rate of 10 L/min. An electric resistance heater placed in the water pipe heats the water from 16 to 43°C. Taking the density of water to be 1 kg/L, determine the electric power input to the heater in kW and the rate of entropy generation during this process in kW/K.
FIGURE P7–209
- (b) In an effort to conserve energy, it is proposed to pass the drained warm water at a temperature of 39°C through a heat exchanger to preheat the incoming cold water. If the heat exchanger has an effectiveness of 0.50 (that is, it recovers only half of the energy that can possibly be transferred from the drained water to incoming cold water), determine the electric power input required in this case and the reduction in the rate of entropy generation in the resistance heating section.
a)
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The electric power input to the heater and the rate of entropy generation during the process.
Answer to Problem 209RP
The electric power input to the heater is
The rate of entropy generation during the process is
Explanation of Solution
Write the expression for the energy balance of steady flow system.
Here, rate of net energy transfer in to the control volume is
Write the expression to calculate the mass flow rate
Here, density of water at room temperature is
Write the expression for the entropy balance equation of the system for steady flow process.
Here, rate of net entropy in is
Conclusion:
There is only one exit and one inlet, write the equation for the mass balance of steady flow system as,
Here, mass flow rate of water at inlet is
The rate of change in internal energy of system inside the system is zero at steady state,
Substitute 0 for
Here, electric power input to the heater is
From Table A-3 “Properties of common liquids, solids and foods”, the value for the density
Substitute
Substitute
Thus, the electric power input to the heater is
Substitute
Since, water is incompressible substance,
Here, rate of entropy generation at stage 1 is
Substitute
Thus, the rate of entropy generation during the process is
b)
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The electric power input required and the reduction in the rate of entropy generation in the resistance heating section.
Answer to Problem 209RP
The electric power input required is
The reduction in the rate of entropy generation in the resistance heating section is
Explanation of Solution
Write the expression to calculate the energy saved
Here, effectiveness of heat exchanger is
Write the expression to calculate the required electric power
Here, electric power input to the heater is
Write the expression to calculate the temperature at which the cold water leaves heat exchanger.
Here, the energy saved is
Write the expression to calulate the entropy generation at stage 2.
Here, rate of entropy generation at stage 2 is
Write the expression to calculate the reduction in the rate of entropy generation within the heating section
Here, reduction in the rate of entropy generation is
Conclusion:
Substitute 0.5 for
Substitute
Substitute
Substitute
Substitute
Thus, the reduction in the rate of entropy generation in the resistance heating section is
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Chapter 7 Solutions
THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<
- Assume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Harrow_forwardAssume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…arrow_forwardAssume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…arrow_forward
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