| Welcome | Navigation | Approach | TEST-Code |
| (The Open Steady daemons build upon the state daemons. Visit States pages first.) |
| States | Closed Process | Closed Steady | |
| Open Process | Closed Cycle | Open Cycles | States-II |
| HVAC | Combustion | Equilibrium | Gas Dynamics |
| (Each section above is divided into two sub-sections - Manual and Applications.) | |
| Manual | |
|
|
(System is open and steady. This page builds upon States pages.)
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.
|
|
| 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.
|
|
|
Step 1: Launch the appropriate device daemon for R-12.
Step 2: Calculate the States.
Step 3: Analyze the Device.
Step 4: Super-Calculate
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%. |
|
| 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.
|
|
|
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 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.
|
|
|
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
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.
|
|
|
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.
|
|
|
Step 1: Launch the appropriate device daemon.
Step 2: Calculate the States.
Step 3: Analyze the Device.
Step 4: Calculate and Super-Calculate
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.
|
|
| 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? |
| Your input! |
For more solved examples on this topic, visit the Home.TEST.Problems pages. If you detect an error or any inconsistent instructions on this page, or would like to see more examples on a particular topic, please write to me using the Home.Comments page. Your input will be appreciated. |
| Manual | |
| Copyright 1998-2003: Subrata Bhattacharjee |