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Daemons>Open Steady> Applications

                                                  EXAMPLE-1
Steam enters steadily a turbine through a duct of diameter 0.2 m. The steam velocity is 90 m/s, the pressure is 14 MPa, and the temperature is 600 oC.  Steam exits the turbine through a duct of diameter 0.8 m with a pressure of 500 kPa and a temperature of 180oC. 

Determine (a) the velocity of the steam at the exit, (b) the mass flow rate in kg/s, (c) the power produced by the turbine if the heat los is 1 MW, and (d) the rate of entropy generation if the ambient temperature is 25oC

What-if scenario: How would the answers change if the exit duct diameter were doubled? 




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click the Load button, and then the Super-Calculate button.
 

 

# HOME>Daemons>Systems>Open>SteadyState>Generic>
# SingleFlow>PhaseChange;

    States { 
             State-1:  H2O;
             Given:       { p1= 14.0 MPa;   T1= 600.0 deg-C; 
                   Vel1= 90.0 m/s;   z1= 0.0 m;   A1= "3.14*.2^2/4" m^2;   }

              State-2:  H2O;
              Given:       { p2= 0.5 MPa;   T2= 180.0 deg-C; 
                        z2= 0.0 m;   mdot2= "mdot1" kg/s; 
                        A2= "3.14*.8*.8/4" m^2;   }
   }

 Analysis {
              Device-A:  i-State =  State-1;  e-State =  State-2; 
              Given: { Qdot= -1000.0 kW;   T_B= 25.0 deg-C;  }
  }
 



Step 1.1: Launch
the appropriate Device
Daemon
 
 
 
 

Step 2: Calculate the i and e States
 
 
 
 
 
 
 
 
 
 

Step 3: Load the States on the Analysis panel, enter device variables, Calculate and Super-Calculate.

Step 4: Change a parameter, Calculate and Super-Calculate.
 

Solution

Answering the six questions described  in the Approach   section leads you to the appropriate daemon page:  HOME. Daemons. Systems. Open. SteadyState. Generic. SingleFlow. PhaseChange . Launch the daemon and choose H2O .

Let  State-1 and State-2 represent the i-State and the  e-State  respectively. 

State-1: Enter A1 as '=3.14*.4*.4/4', Vel1 (90 m/s), p1 (14 MPa),  T1 (600 oC), and   Calculate. The mass flow rate is calculated as 105 kg/s

State-2: Enter A2 as '=3.14*.8*.8/4', p2 (500 kPa),  T2 (180o C), and Calculate. The exit velocity is calculated as 84.8 m/s

On the Analysis panel, load State-1 as the i-State and State-2 as the e-State. Enter the only known device variable Qdot (=-1000 kW) and T_B as 25o C.  A Calculate and Super-Calculate produce Wdot_ext (Other or electrical work) as 81 MW   and  Sdot_gen=29 kW/K  as well as all other process variables. 

For the what-if study, go to States panel,  choose State-2, change the exit area to '=3.14*1.6^2/4', Calculate and   Super-Calculate . All the answers are updated. Note the exit velocity decreases to 21.2 m/s , while the power output is hardly affected with the new value as 81.5 MW.


Fig. 1.1 Image of the Device Panel of the Systems...SingleFlow.H2O  daemon. 


                                                     EXAMPLE-2
Refrigerant-12 enters steadily an adiabatic compressor as a mixture of saturated vapor and saturated liquid with a quality of 95% and pressure 80 kPa at a rate of 1 m3/min, and exits at 2 MPa. The compressor has an adiabatic efficiency of 75%. Assuming the surrounding conditions to be 100 kPa, 25 oC, determine (a) the actual power,  (b) the rate of entropy generation and (c) the second-law efficiency. Neglect KE and PE.

What-if scenario:   (a) How would the answers change if the ambient temperature were 15 oC instead? (b) How would the answers change if R-12 were replaced with R-134a?



 


Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click the Load button, and then the Super-Calculate button.
 

 

# HOME>Daemons>Systems>Open>SteadyState>Generic>
# SingleFlow>PhaseChange;

     States { 
              State-1:  R-12;
             Given:       { p1= 0.08 MPa;   x1= 95.0 %;   Vel1= 0.0 m/s; 
                      z1= 0.0 m;   Voldot1= 1.0 m^3/min;   }

             State-2:  R-12;
            Given:       { p2= 2.0 MPa;   Vel2= 0.0 m/s;   z2= 0.0 m; 
                      j2= "j1-(j1-j3)/0.75" kJ/kg;   }

             State-3:  R-12;
             Given:       { p3= "p2" MPa;   s3= "s1" kJ/kg.K; 
                      Vel3= 0.0 m/s;   z3= 0.0 m;   }
 }

    Analysis {
             Device-A:  i-State =  State-1;  e-State =  State-2; 
             Given: { Qdot= 0.0 kW;   T_B= 25.0 deg-C;   }
 }
 


Step 1: Launch the appropriate device daemon for R-12.
 
 
 
 

Step 2: Calculate the States.
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

Step 3: Analyze the Device.
 
 

Step 4: Super-Calculate 
to obtain State-2.
 
 
 
 

Step 5: Calculate the dead state for availability study.
 
 
 
 
 

Step 6: For the what-if study, change the parameters, Calculate and Super-Calculate.
 

Solution

Answering the six questions described in the Approach   section leads you to the appropriate daemon page:  HOME. Daemons. Systems. Open. SteadyState. Generic. SingleFlow. PhaseChange . Launch the daemon and choose R12 .

Let  State-1 represent the i-State and State-2 represent the e-State. Because the actual exit state is related to an ideal exit  state through adiabatic efficiency, let  State-3 represent that ideal state isentropic to State-1 and isobaric to State-2

State-1: Enter p1 (80 kPa),  x1 (95%), Voldot1 (1m3/min), and   Calculate. Leave Vel1 and z1 at their default value of zero. the mass flow rate is calculated as 0.089 kg/s . Note that the inlet area calculated is ridiculously high. To obtain a realistic A1, Vel1 has to have a realistic value.

State-2: Enter p2 (2 MPa) and leave Vel2 and z2 at their default value of zero. eta_adb=Wdot_ext,s/Wdot_ext = (j1-j3)/(j1-j2). Therefore, j2=j1-(j1-j3)/eta_ad . Enter j2 as '=j1-(j1-j3)/0.75 and  Calculate. The State, obviously cannot be determined because State-3 is completely unknown at this stage. 

State-3: Enter p3  as '=p2',  s3 as '=s1', leave Vel1 and z1 at their default value and   Calculate. The temperature T3 is calculated as 79.4 oC .

On the Analysis panel, load State-1 as the i-State and State-2 as the e-State. Enter the only known device variable Qdot (=0) and T_B as 25oC.  A Calculate and Super-Calculate produce Wdot_ext (the desired compressor power) as -6.44kW   and  Sdot_gen=0.0044 kW/K  as well as all other unknown process and state variables. Go to the States panel to find the final temperature T2 as  100 oC. For availability analysis a dead state, State-0, must be evaluated first. 

State-0: Enter p0 (100 kPa) and T0 (25oC),   and   Calculate. 

On the Availability panel, load State-0 as the dead state. A Calculate produces the second-law efficiency eta_II=79.8%
 

For the what-if study, go to States panel,  choose State-0, change T0 to its new value (15o C) and Calculate . Get back to the Availability panel and do a   Super-Calculate . All the answers are updated. The new value for eta_II=80.4%
For the second part, select the working fluid on the States panel to be R-134a. A Super-Calculate yields: Wdot_ext=-6.19 kW   and Sdot_gen=0.0044 kW/K



 
Fig. 2.1 Image State-2 at the end of all calculations. 



 
                                                 EXAMPLE-3
Air enters an insulated diffuser operating at steady state with a pressure of 80 kPa, a temperature of  0oC and a velocity of 250 m/s. Determine the percent increase in the area necessary to raise the exit pressure to 100 kPa. Assume the diffuser to be reversible and air to have constant specific heats. 

What-if scenario:   (a) How would the answer change if the air temperature were 40 oC instead?




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click the Load button, and then the Super-Calculate button.
 

 

#HOME>Daemons>Systems>Open>SteadyState>
#          Generic>SingleFlow>PerfGas

   States { 
               State-1:  Air;
               Given:       { p1= 80.0 kPa;   T1= 0.0 deg-C; 
                            Vel1= 250.0 m/s;   z1= 0.0 m;   mdot1= 1.0 kg/s;   }

                State-2:  Air;
                Given:       { p2= 100.0 kPa;   z2= 0.0 m;   }
  }

   Analysis {
                Device-A:  i-State =  State-1;  e-State =  State-2; 
                Given: { Qdot= 0.0 kW;   Wdot_ext= 0.0 kW; 
                            T_B= 25.0 deg-C;   Sdot_gen= 0.0 kW/K;   }
  }
 


Step 1: Launch the appropriate Device Daemon
 
 
 
 
 
 
 
 
 
 
 

Step 2: Calculate State-1 and State-2. Assume a unit mass flow rate.
 
 
 
 

Step 3: On the Analysis panel, load the calculated states, enter the known device variables. A Calculate and Super-Calculate produce the desired answers.
 
 

Step 4: Change a parameter, Calculate and Super-Calculate the new answer. Show that answers are independent of the mass flow rate
 
 

 

 Solution

Answering the six questions described in the Approach   section leads you to the appropriate daemon page:  HOME. Daemons. Systems. Open. SteadyState. Generic. SingleFlow. PerfGas .

Let  State-1 and State-2 represent the i-State and the  e-State  respectively. Note that no mass flow rate is given in the problem. We will assume a mdot of 1 kg/s and check that the answers produced by this analysis do not depend on our choice of flow rate.

State-1: Enter p1 (80 kPa), T1 (0oC), Vel1 (250 m/s), mdot1 (1 kg/s) and Calculate. The inlet area A1 is calculated as 39.2 cm2

State-2: Enter p2 (100 kPa), initialize Vel2 (unknown),  and Calculate. The state is, obviously, not fully evaluated. 

On the Analysis panel, load State-1 as the i-State and State-2 as the e-State. Enter the known device variable Qdot (0 kW), Wdot_ext (0 kW), and Sdot_gen (=0 because of no irreversibility). The value of  T_B does not affect the entropy balance equation because the diffuser is adiabatic.  A Calculate and Super-Calculate produce the exit State.

Get back to State-2 to find a completely evaluated state (not the gray background of the properties exported from the Analysis panel). The exit area is calculated as 
 51.5 cm2 , an increase of about 31.4 % . Select State-2 , change mdot1 to 2 kg/s. Update all calculations using a Calculate followed by a Super-Calculate . The inlet and exit areas, both double without affecting the answer.

For the what-if study, change T1 to 40oC. A Calculate and   Super-Calculate  yield A1  and A2 as 44.9 cm2 and 66.0 cm2 respectively, an increase of  47.0 %.
 




 
                                                           EXAMPLE-4
A pump operating at steady state raises oil from 25 ft underground where the pressure is 15 psia and temperature is 20oC, and delivers it 100 ft above ground at a pressure of 60 psia. (a) Determine the minimum pumping power for a mass flow rate of 10 lbm/s.  Neglect any change in kinetic energy and  heat transfer.

What-if scenario: How would the answer change if the supply pressure were reduced to 45 psia?

 




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click the Load button, and then the Super-Calculate button.
 

 

#HOME>Daemons>Systems>Open>SteadyState>
#          Generic>SingleFlow>SolidLiquid

    States { 
          State-1:  Oil(L);
          Given:       { p1= 15.0 psia;   T1= 20.0 deg-C; 
                Vel1= 0.0 ft/s;   z1= -25.0 ft;   mdot1= 10.0 lbm/s;   }

          State-2:  Oil(L);
          Given:       { p2= 60.0 psia;   Vel2= 0.0 ft/s; 
                z2= 100.0 ft;   }
  }

   Analysis {
          Device-A:  i-State =  State-1;  e-State =  State-2; 
          Given: { Qdot= 0.0 Btu/min;   T_B= 77.0 deg-F; 
                Sdot_gen= 0.0 Btu/R.min;   }
  }
 


Step 1: Launch the appropriate device daemon for Liquid
 
 
 
 
 
 
 

Step 2: Calculate the States
 
 

Step 3: Analyze the Device
 

Step 4: Calculate and Super-Calculate 
the desired results
 
 
 
 

Step 5: For the what-if study, change p2, Calculate and Super-Calculate.
 

Solution

Answering the six questions described in the Approach   section leads you to the appropriate daemon page:  HOME. Daemons. Systems. Open. SteadyState. Generic. SingleFlow. SolidLiquid .

Let  State-1 represent the i-State (at the surface of the liquid in the supply reservoir where the pressure and height are known) and  State-2 (at the surface of the water where the pressure and height are known) the e-State . Let us fix the datum at the pump location, i.e., z1=-25 ft . Switch to English system and choose Oil as the working fluid.

State-1: Enter mdot1 (10 lbm/s), p1 (15 psia), T1(20oC),  z1 (-25 ft), and   Calculate. Leave Vel1 at its default value of zero (which produces a ridiculously large A1. For a realistic A1 change Vel1 to a reasonable value).

State-2: Enter p2 (60 psia),  z2 (100 ft), and   Calculate. 

On the Analysis panel, load State-1 as the i-State and State-2 as the e-State. Enter the known device variable Qdot (=0),   Sdot_gen (=0 for a pump with no irreversibility or wasted power), and T_B as 25oC (its value does not affect the calculations as the heat transfer is assumed to be zero).  A Calculate and Super-Calculate produce Wdot_ext=-4.35 hp. Notice that T2 is evaluated as part of the solution. 

For the what-if study, go to States panel,  choose State-2, change p2  to its new value (45 psia) and Calculate . Get back to the Analysis panel and do a   Super-Calculate . All the answers are updated. The new value for Wdot_ext=-3.66 hp.

If the problem involves H2O, the appropriate daemon could be chosen as pure liquid or two-phase mixture. In the second case, liquid can be represented by saturated liquid  (x=0) without any significant error.



 
                                                         EXAMPLE-5
100 m3/min of N2 at 100 kPa, 30 o C is mixed with 50 m3/min of CO2 at 200oC and 100 kPa in an adiabatic mixing chamber. Determine the final temperature and rate of generation of entropy. Assume the gases to behave as ideal gases and no pressure drop in the mixing chamber. Neglect any pressure drop or changes in KE or PE in the mixing chamber.

What-if scenario:   How would the entropy generation change if the pressure inside the chamber were 200 kPa instead?




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click the Load button followed by the Super-Calculate button.
 

 

#  HOME>Daemons>Systems>Open>SteadyState>Generic>
#                                      MultiFlowMixed>IdealGasBinaryMixture;

  States    {  
     State-1:  N2, CO2;
     Given:       { p1= 100.0 kPa;   T1= 29.999994 deg-C;   Vel1= 0.0 m/s;   z1= 0.0 m;   Voldot1= 100.0 m^3/min;   x_A1= 1.0 fraction;   }

     State-2:  N2, CO2;
     Given:       { p2= "p1" kPa;   T2= 200.0 deg-C;   Vel2= 0.0 m/s;   z2= 0.0 m;   Voldot2= 50.0 m^3/min;   x_A2= 0.0 fraction;   }

     State-3:  N2, CO2;
     Given:       { p3= "p1" kPa;   Vel3= 0.0 m/s;   z3= 0.0 m;   x_A3= "mdot1/(mdot1+mdot2)" fraction;   }
    }

  Analysis    {
     Device-A:  i-State =  State-1, State-2;  e-State =  State-3;  Mixing: true;
     Given: { Qdot= 0.0 kW;   Wdot_ext= 0.0 kW;   T_B= 25.0 deg-C;   }
 }

Step 1: Classify the problem and launch the appropriate Device Daemon
 
 
 
 
 

Step 2: Calculate the inlet and exit states
 
 
 
 
 
 
 
 
 
 
 
 

Step 3: On the Analysis panel, load the calculated states, enter the known device variables. A Calculate and Super-Calculate produce the desired answers.
 
 

Step 4: Change a parameter, Calculate and Super-Calculate the new answer.

 Solution

Answering the six questions described in the Approach   section leads you to the appropriate daemon page:  HOME. Daemons. Systems. Open. SteadyState. Generic. FlowMixed. IdealGasMixture .

Let  State-1 and State-2 represent the two inlets, i1-State and the  i2-State  respectively, and State-3 represent the exit inlets, e-State. Choose N2 from the first gas-selector (gas-A) and CO2 from the second gas-selector (gas-B).

State-1: Enter x_A1 (1), T1 (30oC), p1(100 kPa), Voldot1 (100 m3/min), and Calculate. The mass flow rate is calculated as 1.85 kg/s

State-2: Enter x_A2 (0), T2 (200oC), p2('=p1'), Voldot2 (50 m3/min), and Calculate. The mass flow rate is calculated as 0.93 kg/s

State-3: Enter x_A3 ('=mdot1/(mdot1+mdot2)), p3 (=p1), and Calculate. The state cannot be fully evaluated at this stage. 

On the Analysis panel, load State-1 as the i1-State,  State-2 as the i2-State, and  State-3 as the e1-State (note that the daemon can handle up to two exit states). Enter the known device variable Qdot (0 kW) and Wdot_ext (0 kW). The value of  T_B does not affect the entropy balance equation because the chamber is adiabatic.  A Calculate and Super-Calculate produce the exit State and the unknown device variable, Sdot_gen=0.4657 kW/K. Go to the States window to find T3=83.5oC .

For the what-if study, change p1 to 200 kPa. A Calculate and   Super-Calculate  yield Sdot_gen=0.9307 kW/K

The daemon allows two exits, which can be useful for a separator where a single flow enters and separates into two different flows as in a separation chamber used in some refrigeration systems.
 


Fig. 5.1  Image of Device Panel of the mixing daemon. Note that State-e2 is left alone
as there is only one exit in this mixing chamber.



 
                                                       EXAMPLE-6
Air enters a heat exchanger, operating at steady state, at  1 MPa and 600 K at a mass flow rate of 1000 kg/min and leaves without any significant pressure loss. Heat is transferred to the air at a rate of 4000 kW. Nitrogen, flowing separately, enters at 150 kPa and 800 K and leaves at 120 kPa and 600 K. (a) Determine the exit temperature of air,  (b) the mass flow rate of nitrogen and (c) the rate of entropy generation. Neglect any change in kinetic energy and  heat transfer.

What-if scenario: How would the answers change if the heat transfer had to be augmented to 5000 kJ/min?

 




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click Load followed by Super-Calculate.
 

 

#HOME>Daemons>Systems>Open>SteadyState>
#           Generic>MultiFlowUnmixed>IdealGasBinaryMixture

 
 
  States    { 
     State-1:  Air, N2;
     Given:       { p1= 1000.0 kPa;   T1= 600.0 K;   Vel1= 0.0 m/s;   z1= 0.0 m;   mdot1= 1000.0 kg/min;   x_A1= 1.0 fraction;   }

     State-2:  Air, N2;
     Given:       { p2= "p1" kPa;   Vel2= 0.0 m/s;   z2= 0.0 m;   x_A2= "x_A1" fraction;   }

     State-3:  Air, N2;
     Given:       { p3= 150.0 kPa;   T3= 800.0 K;   Vel3= 0.0 m/s;   z3= 0.0 m;   x_A3= 0.0 fraction;   }

     State-4:  Air, N2;
     Given:       { p4= 120.0 kPa;   T4= 600.0 K;   Vel4= 0.0 m/s;   z4= 0.0 m;   mdot4= "mdot3" kg/min;   x_A4= "x_A3" fraction;   }
    }

  Analysis    {
     Device-A:  i-State =  State-1, State-3;  e-State =  State-2, State-4;  Mixing: false;
     Given: { Qdot= 0.0 kW;   Wdot_ext= 0.0 kW;   T_B= 25.0 deg-C;   }

     Device-B:  i-State =  State-1;  e-State =  State-2;  Mixing: false;
     Given: { Qdot= 4000.0 kW;   Wdot_ext= 0.0 kW;   T_B= 25.0 deg-C;   }

     Device-C:  i-State =  State-3;  e-State =  State-4;  Mixing: false;
     Given: { T_B= 25.0 deg-C;   }
    }



Step 1: Launch the appropriate device daemon.
 
 
 
 
 
 
 

Step 2: Calculate the States.
 
 

Step 3: Analyze the Device.
 

Step 4: Calculate and Super-Calculate 
the desired results.
 
 
 
 

Step 5: For the what-if study, change parameter, Calculate and Super-Calculate.
 

Solution

The appropriate daemon is launched from HOME. Daemons. Systems. Open. SteadyState. Generic. FlowUnmixed. IdealGasMixture . Note that a perfect gas is a better choice if the gas is unknown (custom-build with user-specified cp and M ).

In this problem there are essentially three devices.

Device-A : The entire heat exchanger with State-1 representing the i1-State and State-2 the e1-State , State-3 the i2-State and State-4 representing the e2-State

Device-B : The air stream with a single inlet and exit, State-1 representing the i1-State and State-2 representing the e1-State.

Device-C : The nitrogen stream with a single inlet and exit, State-3 representing the i2-State and State-4 representing the e2-State.

State-1 (Air inlet): Select Air as gas-A with x_A=1. Enter p1 (1 MPa), T1(600  K), and mdot1 (1000 kg/min) (leave Vel1 and z1 to their default value of 0)  and  Calculate. 2.87 m3/s

State-2 (Air exit): Enter x_A as '=x_A1' , p2 as '=p1', and mdot2 as '=mdot1'.  Calculate. Note that not much is known about this state

State-3 (N2 inlet): To compose pure N2 out of a mixture, choose N2 as Gas-B and enter x_A=0. Enter  p3 (150 kPa) and T3 (800 K),  and   Calculate.   Note that a j3=h3= 540 kJ/kg

State-4 (N2 exit): Enter x_A4=x_A3. Enter p4 (120 kPa), T4 (600 K),  and   Calculate.   Note that a j4=h4= 319 kJ/kg

On the Analysis panel there are three devices.

Device-A : Load State-1 as the i1-State, State-2 as the e1-State,  State-3 as the i2-State and State-4 as the e2-State. Enter  Qdot (=0, heat transfer in the heat exchanger is interanal), and  Wdot_ext (=0).  Calculate.

Device-B : Load State-1 as the i1-State  and  State-2 as the e1-State. Enter  Qdot (=4000 kW) and  Wdot_ext (=0).  A Calculate and Super-Calculate produce  T2= 822 K, mdot3= 1083 kg/min and Sdot_gen= 1.11 kW/K

Note that we do not need Device-C in this problem. However, if you create Device-C with and enter Wdot_ext=0, you will get Qdot=-4000 kW.

For the what-if study, go to Device-B ,  change Qdot to the new value,  Calculate and    Super-Calculate. All the answers are updated. The new value for T2=874 K . Note that p2 remains an unknown as it depends on the friction inside the tube. If p2 were given, the device variable, Sdot_gen would have been determined.
 


Fig. 6.1 Image of the Device Panel. Note that the Non-Mixing option is selected.


 
                                                       EXAMPLE-7
Air enters a heat exchanger, operating at steady state, at  250 kPa and 127 deg-C at a volume flow rate of 25 m^3/s and exits at 75 deg-C without any loss of pressure. Water, flowing separately, enters at 100 kPa and 25 deg-C and leaves at 100 kPa and 40 deg-C. (a) Determine the mass flow rate of water, and (b) the rate of entropy generation. Neglect heat transfer and any change in ke/pe.

What-if scenario: How would the answers change if the heat exchanger looses heat at the rate of 10 kW? Assume the atmospheric temperature to be 25 deg-C.

 




Time Saver: To reproduce the visual  solution, copy and paste 
this TEST-code on the I/O panel 
of the appropriate daemon, click Load followed by Super-Calculate.
 

 

#HOME>Daemons>Systems>Open>SteadyState>
#           Generic>FlowUnmixed>IG/SL

    States    { 
     State-1:  Air, Water(L);
     Given:       { p1= 250.0 kPa;   T1= 127.0 deg-C;   Vel1= 0.0 m/s;   z1= 0.0 m;   Voldot1= 25.0 m^3/s;   Model1= 1.0 UnitLess;   }

     State-2:  Air, Water(L);
     Given:       { p2= "p1" kPa;   T2= 75.0 deg-C;   Vel2= 0.0 m/s;   z2= 0.0 m;   mdot2= "mdot1" kg/s;   Model2= 1.0 UnitLess;   }

     State-3:  Air, Water(L);
     Given:       { p3= 100.0 kPa;   T3= 25.0 deg-C;   Vel3= 0.0 m/s;   z3= 0.0 m;   Model3= 2.0 UnitLess;   }

     State-4:  Air, Water(L);
     Given:       { p4= "p3" kPa;   T4= 40.0 deg-C;   Vel4= 0.0 m/s;   z4= 0.0 m;   Model4= 2.0 UnitLess;   }
    }

 Analysis    {
     Device-A:  i-State =  State-1, State-3;  e-State =  State-2, State-4;  Mixing: false;
     Given: { Qdot= 0.0 kW;   Wdot_ext= 0.0 kW;   T_B= 25.0 deg-C;   }
    }




The solution procedure is almost identical to the one used in the previous example except the IG/SL model is selected to handle air/water flows.
 
 
 
 
 
 
 
Solution

Modeling the water with the solid/liquid model and air with the ideal gas model, launch the ... Systems. Open. SteadyState. Generic. FlowUnmixed. IG/SL daemon.  

Setup the four states as described in the TEST-Code above. For each state you must select the working fluid carefully. Load the states on the Device Panel, enter Qdot=Wdot_ext=0, Calculate and  Super-Calculate. The mass flow rate of water is found to be 45.78 kg/s and the entropy generation rate 1.71 kW/K .

For the what-if study, go to Device-A ,  change Qdot to -10 kW,  Calculate and    Super-Calculate. The new value for mdot3= 45.6 kg/s. and Sdot_gen= 1.71 kW/K. Could you explain why the entropy generation rate in the system's universe does not show any change?
 





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