Conservation of Energy Approach to System Analysis
1. Setting the facility
- Make sure that the fan is not running, so there is no flow in the facility.
- Verify that the data acquisition system (Figure 4(A)) follows the schematic in figure 2B.
- Connect the positive port of pressure transducer #1 (see figure 2B for reference) to the pressure tap upstream of the valve (
). - Leave the negative port of the pressure transducer #1 open to the room conditions (receiver:
). Hence, the reading of this transducer will be directly 
. - Connect the positive port of pressure transducer #2 (see figure 2B for reference) to the plenum pressure tap (
). - Connect the negative port of pressure transducer #2 (see figure 2B for reference) to the pressure tap upstream of the valve (). Hence, the reading of this transducer will be directly
, as required by equation (10).
- Connect the positive port of pressure transducer #1 (see figure 2B for reference) to the pressure tap upstream of the valve (
- Make sure that the virtual channel 0 in the data acquisition system (Figure 4(B)) corresponds to pressure transducer #1 () and the virtual channel 1 corresponds to pressure transducer #2 ().
- Set the data acquisition system to sample at a rate of 100 Hz for a total of 500 samples (i.e. 5s of data).
Table 1. Basic parameters for experimental study.
|
Parameter |
Value |
| Pipe diameter (D) | 50.8 mm (2 inch) |
| Transducer #1 calibration constant (m_p1) |
|
| Transducer #2 calibration constant (m_p2) |
|
| Local atmospheric pressure | 100,474.15 Pa |
| Local temperature | 297.15 K |
| Local air density | 1.186 kg/m3 |
Figure 4. Flow facility. (A): view of plenum discharge into the receiver section before installing the set of valves to be studied. (B): three different kind of valves inside the receiver. From left to right: gate valve, globe valve, butterfly valve. (C): exit ports from the receiver. The valves discharge the flow inside the receiver, and the fan sucks the flow out of the receiver through the perforated plate in the picture. Please click here to view a larger version of this figure.
2. Measurements
- Record the diameter of the pipe connected to the valve and calculate its cross-sectional area.
- Determine the maximum number of full turns of the handle required to move the valve from the fully closed position to the fully open position. If this number is not an integer, exclude the last fractional rotation to simplify this analysis. For the current experiment, the maximum number of full turns is 12.
- Close the valve completely.
- Rotate the handle of the valve until it is fully open while counting the number of full turns. For simplicity, use only an integer number of turns for the experiment. For example, it takes approximately 12 turns and 1/3 of a turn to fully open the valve used in this experiment. Hence, we will turn the handle of this valve only 12 full turns from its fully closed position and define that as the initial position (
). - Turn the flow facility on.
- Use the data acquisition system to record the readings of and .
- Enter in table 2 the average values of and obtained with the data acquisition system.
- Close the valve by 1.5 turns.
- Repeat steps 2.6 to 2.8 until table 2 is fully populated.
- Turn the flow facility off.
3. Data Analysis
- Determine the loss coefficient of the valve for each angular position using equation (5). Enter these values in table 2.
- Determine the flow rate for each angular position of the valve using equation (10). Enter these values in table 2.
- Determine the operating point using equation (7). Enter these values in table 2.
- Calculate the relative difference between the measured flow rate and the operating point
- Use equation (3) to produce a plot of the system curves for all the values of
. Consider the total loss coefficient as 
. - Add the characteristic curve of the fan to this same plot using equation (2).
Table 2. Representative results. Measurements of pressure differences and estimations of flow rate and loss coefficients.
| [P_pl-P_a ] (Pa) | [P_a-P_r ] (Pa) | Q (m3/s) | K | Q_OP (m3/s) | ε (%) |
| 246.75 | 54.00 | 0.0327 | 0.450 | 0.0316 | -3.16 |
| 208.62 | 114.22 | 0.0301 | 0.976 | 0.0293 | -2.51 |
| 156.19 | 204.80 | 0.0260 | 2.198 | 0.0254 | -2.30 |
| 109.30 | 281.69 | 0.0218 | 4.224 | 0.0214 | -1.53 |
| 71.82 | 348.38 | 0.0176 | 7.863 | 0.0174 | -1.26 |
| 38.72 | 408.60 | 0.0129 | 16.989 | 0.0128 | -0.90 |
| 15.00 | 452.39 | 0.0081 | 48.359 | 0.0080 | -0.32 |
| 2.51 | 482.50 | 0.0033 | 307.799 | 0.0033 | -0.18 |
Source: Ricardo Mejia-Alvarez and Hussam Hikmat Jabbar, Department of Mechanical Engineering, Michigan State University, East Lansing, MI
The purpose of this experiment is to demonstrate the application of the energy conservation equation to determine the performance of a flow system. To this end, the energy equation for steady, incompressible flow is applied to a short pipe with a gate valve. The gate valve is then gradually closed and its influence on flow conditions is characterized. In addition, the interplay between this flow system and the fan that drives the flow is studied by comparing the system curve with the characteristic curve of the fan.
This experiment helps understanding how energy dissipation is used by valves to restrict the flow. Also, under the same principle, this experiment offers a simple method to measure flow rate using the pressure change across a sharp entrance.
1. Setting the facility
- Make sure that the fan is not running, so there is no flow in the facility.
- Verify that the data acquisition system (Figure 4(A)) follows the schematic in figure 2B.
- Connect the positive port of pressure transducer #1 (see figure 2B for reference) to the pressure tap upstream of the valve ().
- Leave the negative port of the pressure transducer #1 open to the room conditions (receiver:). Hence, the reading of this transducer will be directly .
- Connect the positive port of pressure transducer #2 (see figure 2B for reference) to the plenum pressure tap ().
- Connect the negative port of pressure transducer #2 (see figure 2B for reference) to the pressure tap upstream of the valve (). Hence, the reading of this transducer will be directly, as required by equation (10).
- Connect the positive port of pressure transducer #1 (see figure 2B for reference) to the pressure tap upstream of the valve (
- Make sure that the virtual channel 0 in the data acquisition system (Figure 4(B)) corresponds to pressure transducer #1 () and the virtual channel 1 corresponds to pressure transducer #2 ().
- Set the data acquisition system to sample at a rate of 100 Hz for a total of 500 samples (i.e. 5s of data).
Table 1. Basic parameters for experimental study.
|
Parameter |
Value |
| Pipe diameter (D) | 50.8 mm (2 inch) |
| Transducer #1 calibration constant (m_p1) |
|
| Transducer #2 calibration constant (m_p2) |
|
| Local atmospheric pressure | 100,474.15 Pa |
| Local temperature | 297.15 K |
| Local air density | 1.186 kg/m3 |
Figure 4. Flow facility. (A): view of plenum discharge into the receiver section before installing the set of valves to be studied. (B): three different kind of valves inside the receiver. From left to right: gate valve, globe valve, butterfly valve. (C): exit ports from the receiver. The valves discharge the flow inside the receiver, and the fan sucks the flow out of the receiver through the perforated plate in the picture. Please click here to view a larger version of this figure.
2. Measurements
- Record the diameter of the pipe connected to the valve and calculate its cross-sectional area.
- Determine the maximum number of full turns of the handle required to move the valve from the fully closed position to the fully open position. If this number is not an integer, exclude the last fractional rotation to simplify this analysis. For the current experiment, the maximum number of full turns is 12.
- Close the valve completely.
- Rotate the handle of the valve until it is fully open while counting the number of full turns. For simplicity, use only an integer number of turns for the experiment. For example, it takes approximately 12 turns and 1/3 of a turn to fully open the valve used in this experiment. Hence, we will turn the handle of this valve only 12 full turns from its fully closed position and define that as the initial position ().
- Turn the flow facility on.
- Use the data acquisition system to record the readings of and .
- Enter in table 2 the average values of and obtained with the data acquisition system.
- Close the valve by 1.5 turns.
- Repeat steps 2.6 to 2.8 until table 2 is fully populated.
- Turn the flow facility off.
3. Data Analysis
- Determine the loss coefficient of the valve for each angular position using equation (5). Enter these values in table 2.
- Determine the flow rate for each angular position of the valve using equation (10). Enter these values in table 2.
- Determine the operating point using equation (7). Enter these values in table 2.
- Calculate the relative difference between the measured flow rate and the operating point
- Use equation (3) to produce a plot of the system curves for all the values of . Consider the total loss coefficient as .
- Add the characteristic curve of the fan to this same plot using equation (2).
Table 2. Representative results. Measurements of pressure differences and estimations of flow rate and loss coefficients.
| [P_pl-P_a ] (Pa) | [P_a-P_r ] (Pa) | Q (m3/s) | K | Q_OP (m3/s) | ε (%) |
| 246.75 | 54.00 | 0.0327 | 0.450 | 0.0316 | -3.16 |
| 208.62 | 114.22 | 0.0301 | 0.976 | 0.0293 | -2.51 |
| 156.19 | 204.80 | 0.0260 | 2.198 | 0.0254 | -2.30 |
| 109.30 | 281.69 | 0.0218 | 4.224 | 0.0214 | -1.53 |
| 71.82 | 348.38 | 0.0176 | 7.863 | 0.0174 | -1.26 |
| 38.72 | 408.60 | 0.0129 | 16.989 | 0.0128 | -0.90 |
| 15.00 | 452.39 | 0.0081 | 48.359 | 0.0080 | -0.32 |
| 2.51 | 482.50 | 0.0033 | 307.799 | 0.0033 | -0.18 |
Conservation of energy is a well established physical principle that is frequently applied in the design and analysis of mechanical systems. Since energy is conserved, careful accounting of how it is added to and dissipated from a system as well as the internal transformations to the various forms can yield important details about the operating conditions. The advantage of this approach is that it often allows many details of the system to be ignored. So, the analysis can be greatly simplified. This video will illustrate the application of conservation of energy to a flow system with a gate valve. And show how this approach can be used to determine the operating point of the system as well as the loss coefficient of the valve.
Consider the flow facility shown in this schematic. Air is drawn into the plenum from atmospheric conditions and flows into the receiver room through a short pipe section with a sharp entrance, a gate valve, and an open discharge. The air then flows through an orifice plate and a centrifugal fan before returning to atmospheric conditions. The total energy carried by the flow is a combination of kinetic, potential, and thermodynamic components as shown in the equation for the specific energy at a point in the flow. These components can freely transform from one type to another through the system. Note that alpha is a correction factor to take into account that the velocity is not constant across the flow section. For turbulent flow, alpha is usually taken as one. And for laminar flows, it is noticeably larger. In pipe flows at moderate Reynolds numbers, alpha is approximately 1.1. Since energy is conserved, any difference in the specific energy between two points in the flow must be the result of external work on the fluid or dissipation. Additionally, if analysis is restricted to points at the same height, the gravitational potential will not contribute to the difference. This is the energy equation for the system. Now consider the system losses. The most significant losses will occur at the pipe entrance, the valve, and the discharge. These losses are proportional to the kinetic energy of the flow and can be related to the flow rate using continuity. It can be shown that the loss coefficient for the entrance and discharge are one half and one respectively. Consider what happens as the air flows from the plenum into the pipe section. No energy is added, but there is some dissipation at the entrance. Additionally, since the flow velocity in the plenum is negligible compared to the velocity in the pipe section, it can be ignored. The remaining terms can be rearranged to yield the flow rate in terms of the pressure difference between those points. Now consider the pressure drop from the pipe section upstream of the valve to the receiver. Again, no energy is added and losses will occur at the valve and discharge. Flow velocity in the receiver is negligible compared to the pipe section, so the equation simplifies again. In this case, the valve loss is a function of flow rate and the pressure difference can be determined. Finally, consider the whole system. The fluid enters and exits the system at the same pressure and velocity. So the work added by the shaft must be equal to the total losses in the system. If the performance curve of the fan is known, then the operating point, or expected flow rate of the system can be predicted for a given total loss factor. The operating point can be determined graphically by plotting the fan performance curve with the system performance curve. At a given flow rate, the fan curve represents the specific energy added in terms of a pressure jump, while the system curve represents the specific energy loss. At a steady state, these two contributions must be equal. Now that you understand how to use conservation of energy to analyze the system, let's use this technique to calibrate the valve and determine the operating point.
Before you begin setting up, familiarize yourself with the layout and safety procedures of the facility. Check that the fan is not running and there is no flow through the test area. Now set up the data acquisition system as shown in the diagram in the text. Connect the plenum pressure tab to the positive port of pressure transducer two. And then connect the pressure tab upstream of the valve to the negative port of transducer two as well as the positive port of transducer one. Leave the negative port of transducer one open to room conditions. The data acquisition software ensure that virtual channel zero and one correspond to pressure transducers one and two respectively. Finally, set the sampling rate to 100 hertz and total samples to 500. After the data acquisition system is set up, measure the inner diameter of the test pipe and calculate its cross sectional area. Next, turn the valve handle clockwise until the valve is completely closed. And then open the valve by one full turn of the handle at a time keeping count of the number of whole turns required to fully open the valve. If there is a partial turn remaining, return the handle to the nearest full turn. Pick a convenient increment based on the number of turns just counted. For example, if the number of turns was 12, an increment of 1.5 turns gives eight test points from fully open to almost fully closed. Leave the valve in the fully opened position and turn the flow facility on. Now, use the data acquisition system to determine the average pressure differences measured by both transducers at this valve position and record these values. Close the valve by one increment and repeat the measurement. Continue closing the valve by increments and taking measurements until the valve is almost fully closed. When all of the data has been collected, turn the flow facility off.
At each valve position measured by the number of turns from the fully opened position, you have a measurement of the pressure differences between the plenum and the pipe section upstream of the valve and the measurement of the pressure difference between the pipe section upstream of the valve and the receiver. Perform the following calculations for each position of the valve. First calculate the flow rate from the pressure drop between the plenum and the upstream pipe section using the equation derived earlier. Once the flow rate is known, the loss coefficient of the valve can be calculated from the pressure drop between the upstream pipe section and the receiver. Use the loss coefficient to determine the operating point or the expected air flow at this valve position. Finally, compare the operating point to the experimental flow rate by calculating the relative difference between the two. Now look at your results.
Plot the characteristic curve described in the text for the fan and then add the system curves for the total losses at each position of the valve. Both the slope of the system curve and the loss coefficient of the valve increases the valve is closed demonstrating an increase in energy dissipation as the flow is restricted. Conceptually, as KV approaches infinity, all of the energy is dissipated in the valve. In the range of flow rates observed, the percent error is low but always underestimated. Additionally, the error decreases as the valve is closed. This behavior is expected since the correction factor alpha increases slightly with the Reynolds number.
Conservation of energy is frequently used to analyze complex engineering systems. The kinetic energy carried by the wind can be harvest by wind turbines to produce electric power. By comparing upstream with downstream flow conditions, the energy equation can be used to assess how much energy has been removed from the wind. The magnitude of the energy recovered will be given by the shocked work. Change is gravitational potential energy can be used to assess the flow rate of water over a spillway. This is done in combination with the mass conservation equation by measuring the depths upstream and downstream of the spillway.
You've just watched the Jove's introduction to conservation of energy analysis. You should now understand how to apply an energy equation to a flow system, calibrate loss coefficients, and determine the operating point. Thanks for watching.
Figure 5 shows the results for the current measurements. Here, the black solid line was generated with equation (2), and each red line with equation (3) for different values of the valve's loss coefficient. From the figure, it is evident that the system curve increases its slope as the valve closes. In other words, this experiment demonstrates that the principle behind the operation of a valve is to increase energy dissipation to restrict the flow. On the other hand, from...
This experiment explored the application of the energy equation to characterize the action of a valve on pipe flow. It was observed that the valve induces flow resistance by increasing energy dissipation. Considering that the pressure drop along the flow system is directly proportional to the square of the flow rate, the effect of energy dissipation is captured by the magnitude of the proportionality coefficient. This coefficient is the addition of the loss coefficients of all the elements in the flow system, including t...
Chapters in this video
0:07
Overview
1:00
Principles of Conservation of Energy Analysis
4:52
Preparing the Flow Chamber
7:11
Data Analysis
8:17
Results
9:07
Applications
9:55
Summary
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