Changing Patterns of the Flow Ratio with the Distance of Exhaust and Supply Hood in a Parallel Square Push-Pull Ventilation
Abstract
:1. Introduction
2. Subjects and Methods
2.1. Geometric Models
2.2. Research Conditions
- ρ—gas density, kg/m3. The gas density of air is 1.205 kg/m3 at 20 °C used in this study.
- v—hood face velocity, m/s. See Table 1.
- d—hydraulic diameter, m. It is 0.7 m for the push hood and pull hood in this study.
- η—dynamic viscosity, Pa·s. The dynamic viscosity of air is 1.81 × 10−5 Pa·s at 20 °C used in this study.
3. Results
3.1. Results of the Optimal k Value at Different Distances (L/a)
3.2. Results of the Longest Control Distance (L/a) for Parallel Square Push-Pull Ventilation
3.3. Changing Patterns of k Value with L/a When 1.5 ≤ L/a ≤ 5
4. Discussion
- (1)
- The results of this study are based on the square hood. If the hood is circular or rectangular, it may be estimated by equivalent diameter according to the results in Reference [1] and modified appropriately.
- (2)
- There is a worktable between the push and pull hood without flange. If a change is found in the model, the results of the study should be applied with appropriate modifications.
- (3)
- This study does not consider the influence of disturbing the air flow, but it may exist in practice. The size and position of contaminants in practice may have some deviation from the model in this study. Therefore, the results of this study should be applied with appropriate modifications in those above cases.
5. Conclusions
- (1)
- When L/a is 6 or more, a parallel push-pull ventilation is not suitable for use.
- (2)
- The relationship between k and L/a for a parallel push-pull ventilation can be expressed in the equation of k = 0.1675(L/a)3 − 1.318(L/a)2 + 3.6085(L/a) − 1.5352, when 1.5 ≤ L/a ≤ 5.0.
- (3)
- If L/a is known, a relatively accurate k value can be determined by using Equation (3), presented in this study, which can be used in the design of a parallel push-pull ventilation system. When the actual situation and the conditions of this study are different, the appropriate amendments should be made.
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
References
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Push Hood Face Velocity (v1, m/s) | Flow Ratio (k) | Pull Hood Face Velocity (v2, m/s) | Turbulence Intensityof Outlet (I, %) | Reynolds Number of Outlet (Re) |
---|---|---|---|---|
0.50 | 1.0 | 0.50 | 4.55% | 2.33 × 104 |
0.50 | 1.2 | 0.60 | 4.45% | 2.80 × 104 |
0.50 | 1.5 | 0.75 | 4.33% | 3.50 × 104 |
0.50 | 1.7 | 0.85 | 4.26% | 3.96 × 104 |
0.50 | 2.0 | 1.00 | 4.17% | 4.66 × 104 |
0.50 | 2.2 | 1.10 | 4.12% | 5.13 × 104 |
0.50 | 2.3 | 1.15 | 4.10% | 5.36 × 104 |
0.50 | 2.5 | 1.25 | 4.06% | 5.83 × 104 |
0.50 | 2.7 | 1.35 | 4.02% | 6.29 × 104 |
0.50 | 3.0 | 1.50 | 3.97% | 6.99 × 104 |
0.50 | 3.1 | 1.55 | 3.95% | 7.22 × 104 |
0.50 | 3.6 | 1.80 | 3.88% | 8.39 × 104 |
0.50 | 4.0 | 2.00 | 3.83% | 9.32 × 104 |
0.50 | 4.3 | 2.15 | 3.79% | 1.00 × 105 |
0.50 | 4.5 | 2.25 | 3.77% | 1.05 × 105 |
0.50 | 5.0 | 2.50 | 3.72% | 1.17 × 105 |
0.50 | 8.0 | 4.00 | 3.51% | 1.86 × 105 |
0.50 | 10.0 | 5.00 | 3.41% | 2.33 × 105 |
Boundary Conditions | Define |
---|---|
Inlet | Push hood face |
Inlet boundary type | Velocity-inlet |
Velocity inlet (m/s) | 0.5 |
Material | air |
Air viscosity (kg/(m·s)) | 1.81 × 10−5 |
Hydraulic diameter of inlet (m) | 0.7 |
Turbulence intensity of inlet (%) | 4.55 |
Outlet | Pull hood face |
Outlet boundary type | Velocity-inlet |
Velocity outlet (m/s) | See Table 1 |
Turbulence intensity of outlet (%) | See Table 1 |
Species mass fractions | C7H8 0.9 |
Mass flow rate (mg/s) | 500 |
Species transport | On |
Solver type | Pressure-based |
Solver velocity formulation | Absolute |
Solver time | Steady |
Viscous model | standard k-ε |
Energy | On |
Pressure-velocity coupling scheme | SIMPLEC |
Discrete format | Second order upwind |
Convergence criterion | 10−6 |
Interaction to plot and store | 1000 |
No. | L/a | k Value Research Range | Optimal k Value |
---|---|---|---|
1 | 1.5 | 1.0, 1.2, 1.5, 1.7, 2.0 | 1.5 |
2 | 2.0 | 1.0, 1.5, 1.7, 2.0, 3.0 | 1.7 |
3 | 3.0 | 1.5, 1.7, 1.9, 2.0, 2.3, 2.7 | 2.0 |
4 | 4.0 | 1.5, 2.2, 2.3, 2.5, 2.7, 3.0 | 2.5 |
5 | 5.0 | 2.7, 3.1, 3.6, 4.0, 4.5, 5.0 | 4.5 |
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Chen, J. Changing Patterns of the Flow Ratio with the Distance of Exhaust and Supply Hood in a Parallel Square Push-Pull Ventilation. Int. J. Environ. Res. Public Health 2022, 19, 2957. https://doi.org/10.3390/ijerph19052957
Chen J. Changing Patterns of the Flow Ratio with the Distance of Exhaust and Supply Hood in a Parallel Square Push-Pull Ventilation. International Journal of Environmental Research and Public Health. 2022; 19(5):2957. https://doi.org/10.3390/ijerph19052957
Chicago/Turabian StyleChen, Jianwu. 2022. "Changing Patterns of the Flow Ratio with the Distance of Exhaust and Supply Hood in a Parallel Square Push-Pull Ventilation" International Journal of Environmental Research and Public Health 19, no. 5: 2957. https://doi.org/10.3390/ijerph19052957
APA StyleChen, J. (2022). Changing Patterns of the Flow Ratio with the Distance of Exhaust and Supply Hood in a Parallel Square Push-Pull Ventilation. International Journal of Environmental Research and Public Health, 19(5), 2957. https://doi.org/10.3390/ijerph19052957