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American Institute of Aeronautics and Astronautics
An investigation of Air Curtains Flows Effects on heat and
mass transfer Characteristics in a cold room
Dr.Gamal ElHariry, Eng. Ahmed AbuZeid, Prof.Dr.Essam E. Khalil*
Faculty of Engineering, Cairo University, Egypt, *khalile1@asme,org
The main purpose of the present paper is to demonstrate the importance of air curtains on the
likely performance of cold rooms .The paper explores the benefits of using computational fluid
dynamics (CFD) as a tool for simulation of the flow and heat transfer characteristics of air curtains
in a vertical display case and cold rooms .This can be achieved by using computational fluid
dynamics software to simulate the air flow pattern and the temperature distribution in a frozen
food vertical display cabinet .Previous research work is analyzed and critically viewed in respect
of previous literature reported to predict the sensible heat transfer across the air curtain and using
it to investigate the effect of various design parameters such as jet angles and initial velocities on
heat transfer . The present work emphasized the importance of the three dimensional modelling of
the flow regimes downstream of an air curtain used to restrict cold room infiltration. The present
work highlights the significance of using a full three dimensional procedure, using a commercial
CFD code "Fluent 6.2." and gives examples of comparisons with relevant experimentations. The
effect of operating parameters (outlet velocity, temperature and humidity ratio) on the performance
of the air curtain is investigated together with the external wind velocity and curtain outlet angle
.Few published test cases were used to access the validity of the model assumptions and good
agreements with the experiments were generally shown.
Keywords: air curtain, plane free jet, velocity profile, temperature profile, humidity ratio profile
I. Introduction
When opened a door separating a cold storage area from a warm room permits a substantial loss of refrigerated air.
Warm air flows into the cold room through the lower part. This results in energy losses, safety hazards in the form of
condensation and icing on the floor and fog in the doorway; and possibly food spoilage. Strip doors used on coolers
and freezers to reduce these effects impair visibility and are unpleasant to pass through due to condensation and
frosting and accumulate dirt and possible bacterial growth. Studies have proven that Air Curtains, when properly
sized and adjusted, are up to 85% efficient in controlling the flow of air through cooler and freezer doorways. If the
cold storage door is open over one hour per day the Air Curtain is a cost effective way to save refrigeration costs1-10
.
Installed on the warm side of the doorway the Air Curtain emits an air stream which reaches the floor at an angle
and splits into two separate air streams. By properly adjusting the volume of the air and the angle of the nozzle, one
air stream would balance against the other which is trying to leave the cooled room, while the other counteracts the
warm air trying to enter. The correct Air Curtain sizing and adjustments must be made for each specific application
so that a narrow, high velocity, low volume stream of air is projected over the entire opening creating a sufficiently
stiff curtain of air. Built-in adjustments in the Air Curtain must include fully adjustable mounting brackets, variable
volume controls and individually adjustable louvers in the nozzle. The narrow nozzle limits the amount of air in the
doorway area and hence the turbulence, thus increasing the efficiency of the unit. In addition to providing a
substantial energy savings and increased safety, Cold Storage Air Curtains can increase the time between defrosting
by a factor of four, depending on the particular freezer or cooler4. Also, their ability to maintain the cold room
temperature right up to the doorway improves product quality and increases the useful floor space.
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit25 - 28 July 2010, Nashville, TN
AIAA 2010-6931
Copyright © 2010 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
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American Institute of Aeronautics and Astronautics
The benefits of air curtains can be listed as
▪ Increased employee comfort.
▪ Energy savings through control of air transfer
▪ Faster and safer traffic flow and increased production due to clear and open doorways. Door maintenance cost savings due to decreased breakdowns. ▪ Increased usable space near door areas.
▪ Elimination of ice and fog in cold storage areas.
▪ Increased safety in door areas due to better visibility
II. Mathematical Modelling and Assumptions
The present numerical investigation was based on solving the governing equations that described airflow inside the
cold room by a CFD program FLUENT 6.2 5(commercially available CFD program). This numerical approach
solves the partial differential equations governing the transport of mass, three momentum, energy and species in a
fully turbulent three dimensional domain under steady state conditions in addition to standard k – ε model equations
for turbulence closure6-7
.
Computational Fluid Dynamics Models
The different governing partial differential equations are typically expressed in a general form as:
ΦΦΦΦ +
∂
Φ∂Γ
∂
∂+
∂
Φ∂Γ
∂
∂+
∂
Φ∂Γ
∂
∂=Φ
∂
∂+Φ
∂
∂+Φ
∂
∂S
zzyyxxW
zV
yU
xeffeffeff ,,,ρρρ
(1)
Where ρ is the air density and Φ is the dependent variable, SΦ = Source term ofΦ, and U, V, W are the velocity
vectors, and ΓΦ,eff is the effective diffusion coefficient. The effective diffusion coefficients and source terms for the
various differential equations8 are listed in the table 1.
Table 1. Terms of Partial Differential Equations (PDE) equation 1.
Φ ΓΦ,eff SΦ
Continuity 1 0 0
X-momentum U µeff -∂P/∂x +ρg+ SU
Y-momentum V µeff -∂P/∂y+ρg (1+β∆t) + SV
Z-momentum W µeff -∂P/∂z+ρg+ SW
H-equation H µeff/σH SH
RH-Equation RH µeff/σRH SRH
τ-age equation τ µeff/στ ρ k-equation k µeff/σk G - ρ ε ε-equation ε µeff/σε C1 ε G/k – C2 ρ ε2
/k
µeff = µlam + µ t µ t = ρ Cµ k2 / ε
G = µt [2{(∂U/∂x)2 +(∂V/∂y)
2 +(∂W/∂z)
2}+(∂U/∂y + ∂V/∂x)
2 +(∂V/∂z + ∂W/∂y)
2 +(∂U/∂z + ∂W/∂x)
2]
SU = ∂/∂x(µeff ∂Φ/∂x)+∂/∂y(µeff ∂Φ/∂x)+∂/∂z(µeff ∂Φ/∂x)
SV = ∂/∂x(µeff ∂Φ/∂y)+∂/∂y(µeff ∂Φ/∂y)+∂/∂z(µeff ∂Φ/∂y)
SW = ∂/∂x(µeff ∂Φ/∂z)+∂/∂y(µeff ∂Φ/∂z)+∂/∂z(µeff ∂Φ/∂z)
SH is the source of Energy at nodal points
Turbulence model constants C1 = 1.44, C2 = 1.92, Cµ = 0.09
σH = 0.9, σRH = 0.9, στ = 0.9, σk = 0.9, σε = 1.225
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Boundary Conditions
The solution of the governing equations can be realized through the specifications of appropriate boundary
conditions. The values of velocity, temperature, kinetic energy, and its dissipation rate should be specified at all
boundaries. A non-slip condition at all solid walls is applied to the velocities. The logarithmic law of the wall (wall
function) of Launder and Spalding6
was used here, for the near wall boundary layer. At inlets, the air velocity was
assumed to have a uniform distribution; inlet values of the temperature were assumed to be of a constant value and
uniform distribution. All velocity components were set as zeros initially, and temperatures were assumed to be equal
to the steady state value of the comfort condition.
Numerical Procedure
The Computer Program, FLUENT 5 was used to solve the time-independent (steady state) conservation
equations together with the standard k-ε model as Launder and Spalding 6
and the corresponding boundary
conditions. The numerical solution grid divided the space of the cold room into discretized computational cells of
the order of 500,000 tetrahedral cells. The discrete finite difference equations were solved with the SIMPLE
algorithm, Khalil11
. Solution convergence criteria, was applied at each iteration and ensured the summations of
normalized residuals were less than 0.001 for flow, 0.001 for k andε, and 10-6
for energy. The predictions of flow
and turbulence characteristics are in general qualitative agreement with the corresponding experiments and
numerical simulations published by others, Neilsen4. Nevertheless discrepancies exist and particularly in the vicinity
of recirculation zone boundaries. More discrepancies were also observed in situation with heating flows than those
of ventilation or cooling.
Convergence and Stability
The simultaneous and non-linear characteristics of the finite difference equations necessitate that special measures
are employed to procure numerical stability (convergence); these include under relaxation of the solution of the
momentum and turbulence equations by under relaxation factors which relate the old and the new values of Φ as
follows,
( ) oldnew 1 Φγ−+Φγ=Φ
(2)
Where γ is the under-relaxation factor. It was varied between 0.2 and 0.3 for the three velocity components as the
number of iteration increases. For the turbulence quantities, γ was taken between 0.2 and 0.4 and for other variables
between 0.2 and 0.6. The required iterations for convergence are based on the nature of the problem and the
numerical conditions (grid nodes, under-relaxation factor, initial guess, etc.). So the time (on the computer
processor) required to obtain the results is based on many factors. The computational number of iterative steps is
selected according to space cell (spatial difference) to yield converged solutions11
. The validity of the present
computational technique was assessed previously in the open literature, for example Khalil 3, 7
; where reference
should be made for more detailed readings.
III. Results and Discussions
A typical orthogonal three dimensional grid composed of 1070775 mesh cells was used to obtain grid independent
results .The Random Access Memory (RAM) required for the numerical grid depends mainly on the selected CFD
code, grids between 100,000 and 1000,000 mesh cells will require between 40 and 300 Mb of RAM.
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Cold store Model description
Mini type constructional cold store was chosen as a study room and is schematically shown in figure 1. Its exterior
dimension is 4.8 m (L) x 5.8 m (W) x 3.8 m (H). The thickness of the wall of cold store is 150 mm, which is made
up of polystyrene foam. This outside-cold room was modelled by entrance zone that have the same dimensions of
cold room 4.8 m (L) x 5.8 m (W) x 3.8 m (H). The room had an entrance (W x H = 1.36 m x 3.2 m) with a 0.15 m
doorframe .These are typical dimensions of commercial cold rooms commonly used for food storage.
Figure 1. Cold Room Arrangement
A typical industrial air curtain was considered here designed to be installed on doors of cold stores and freezers;
which has low noise centrifugal double inlet fans driven by an external rotor motor with built in thermal protection
contact and is provided with five speed selection device. The unit had perforated inlet grille with large absorbing
surface to minimize the air pressure drop. It does not need filter. The air curtain simulated here, shown in Figure 2,
had the following Specifications:
Airflow: 1000 m3/hr
Fans power input 230v-50Hz: 0.372 KW
Noise level: 53 dB
Weight: 29 kg
Figure2. Air Curtain Design, L=1.0 m
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Boundary Conditions:
1. Inlet Air Conditions:
The inlet air conditions to the air curtain are taken as the average day maximum of 35ºC and 56% relative humidity,
representing July conditions in Cairo. The inlet air condition to the air curtain is modelled as pressure outlet with
target mass flow rate equals to 0.4424 kg/s in negative x-direction since pressure outlet boundary conditions are
used to define the static pressure at flow outlets (and also other scalar variables, in case of backflow). The selected
flow rates and velocities refer to local practice in Egyptian cold rooms designs. The use of a pressure outlet
boundary condition instead of an outflow condition often results in a better rate of convergence when backflow
occurs during iteration.
2. Outlet air conditions
The outlet air condition from the air curtain is modelled as velocity inlet boundary condition with air velocity that
equal to 6 m/s
3. Walls
The walls of cold rooms are to be set at – 20°C which correspond to the inside condition of the cold room. Also it is
assumed that the walls have relative humidity of 90 % which correspond to the inside condition of the cold room as
most of foodstuffs storage conditions lie between 85 and 95 % relative humidity 12
.The no slip condition is enabled
for all walls, while using the standard wall function for near wall treatment. The walls of modelled entrance hall are
to be set at 35°C which correspond to the outside condition of the cold room. Also it is assumed that in the wall
vicinity the relative humidity is 56 % which correspond to the outside condition of the cold room12
.
Modelled Case studies:- Case 1: air curtain discharge is considered as planer jet with axial velocity of 6 m/s in the negative y – direction.
Case 2: air curtain discharge is considered as planer jet with axial velocity of 6 m/s with 15º toward the cold room
Figure 3 and 4 show the air temperature contours as well as the velocity contours identifying some dead zones where
no significant circulation velocity was observed for case 1 along X-axis at X= 1.18 m; at the middle of the air
curtain.
Figure 3. (Case 1) Temperature contours (K), vertical X-Y plane at Z = 1.18 m.
Cold Room
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American Institute of Aeronautics and Astronautics
Figure 4. (Case 1) velocity contours (m/s), vertical X-Y plane at Z = 1.18 m.
Figure 5 shows the humidity ratio contours for case 1 along X-axis at z = 1.18 m; at the middle of the air curtain.
Food stuff should be ideally preserved at low moisture content as explained in boundary conditions; this was not
achieved completely as shown in Figure 5; it can be seen that some zones in the cold room have higher moisture
content which occur due to moisture migration from the outside of cold room to the inside of the room due to the
difference in vapour pressure. This pressure difference draws outside ambient air into the store, with its associated
moisture. Air also infiltrates into the store from door openings where high velocity air currents can be created.
Figure 5. (Case 1) Humidity ratio distribution (kgv/kga), Y-X plane at Z = 1.18 m.
Different velocity, temperatures and water vapour content contours at Y-Z plane at X=5.07 m are shown hereafter in
Figures 6, 7 and 8.The predictions clearly identified the air curtain effects on the velocity contours in door vicinity
as well as the effects on the air thermal pattern and relative humidity values near the door where the air curtain is
located. Such effect would have strong influence on the validity of the food stuff stored in the cold room.
Dead zones
Cold Room
Cold Room
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Figure 6. (Case 1) velocity contours (m/s), vertical plane at X = 5.07 m.
Figure 7. (Case 1) Temperature contours (K), vertical plane at X = 5.07 m.
Figure 8. (Case 1) Humidity ratio distribution (kgv/kga), vertical plane at X = 5.07 m.
Cold Room
Cold Room
Cold Room
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American Institute of Aeronautics and Astronautics
For Case 2, figures 9 and 10 show the air temperature contours as well as the velocity contours identifying some
dead zones where no significant circulation velocity was observed for case 2 along X-axis at X= 1.18 m. At the
middle plane of the air curtain; the tilting the air jet towards the cold room by an angle 15 o resulted in directing the
jet through (pass) into the cold room.
Figure 9. (Case 2) Temperature contours, vertical plane at z = 1.18 m.
Figure 10. (Case 2) velocity contours along the X-axis, vertical plane at z = 1.18 m.
Dead zones
Cold Room
Cold Room
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American Institute of Aeronautics and Astronautics
Figure 11 shows the humidity ratio contours for case 2 along X-axis at z = 1.18 m. The tilting of the air curtain jet
resulted in better preservation of the cold room product as no cold air is allowed to exit. Food stuff should be ideally
preserved at low moisture content as explained in boundary conditions; this was better achieved here than earlier in
Figure 5.
Figure 11. (Case 2) Humidity ratio distribution (kgv/kga), vertical plane at z = 1.18 m.
Different velocity, temperatures and water vapour content contours at Y-Z plane at X=5.07 m are shown hereafter in
Figures 12, 13 and 14.The predictions clearly identified the air curtain effects on the velocity contours in door
vicinity as well as the effects on the air thermal pattern and relative humidity values near the door where the air
curtain is located. Such effect would have strong influence on the validity of the food stuff stored in the cold room.
Figure 12. (Case 2) Temperature contours (K), vertical plane at x = 5.07 m.
Cold Room
Cold Room
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Figure 13. (Case 2) velocity contours (m/s), vertical plane at x = 5.07 m.
Figure 14. (Case 2) Humidity ratio distribution (kgv/kga), vertical plane at x = 5.07 m.
IV.Concluding Remarks
This paper is a preliminary attempt to investigate the flow patterns, thermal characteristics and humidity variation in
a cold room with the use of air curtain. This work is based on the finite difference technique to predict flow
parameters of a single air curtain unit. The present model made use of a commercially available CFD program that
was found to adequately predict the air curtain effects on room air flow patterns. On the basis of the results
demonstrated here, one can recommend the use of such numerical tool to design a cold room air flow pattern to
Cold Room
Cold Room
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control the flow regimes, thermal distribution and relative humidity; these are major factors in efficient cold room
design and operation.
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2Khalil, E. E., 2008, Efficient Energy Utilization in Air Conditioned Buildings in Egypt: New Directive”
THETACONF II, PP.527-532, Cairo, December 2008, EGYPT
3Khalil, E. E., 2000, Computer aided design for comfort in healthy air conditioned spaces, Proceedings of Healthy
Buildings 2000, Finland, Vol. 2, pp 461-466. 4Nielsen, P. V., 1989, Numerical Prediction of air distribution in rooms, ASHRAE, Building Systems: room air and
air contaminant distribution, 1989. 5FLUENT 6.2 Documentation,
© Fluent Inc. 2005.
6Launder, B. E., and Spalding D. B., 1974, The Numerical Computation of Turbulent Flows, Computer Methods
App. Mech., pp. 269-275.
7Khalil.E.E. 2009, Air Conditioning and Refrigeration Designs for Environmental Sustainability, Proceedings of
ICGSI, AC01, Thailand, December 2009 8Spalding, D. B., and Patankar, S. V., 1974, A Calculation Procedure for Heat, Mass and Momentum Transfer in
Three Dimensional Parabolic Flows, Int. J. Heat & Mass Transfer, 15, pp. 1787. 9Elasfouri, A.S. , Abou El-Kassem,E.K and Taha.S.R.,2009, Flow Field Characteristics of a Single Plane Jet Air
Curtain Directed Vertically Downward at Opening between two Non-Isothermal Zones,IECEC Paper number:
AIAA-2009-4512. 10
Elasfouri, A.S. , Abou El-Kassem,E.K and Taha.S.R.,2009Heat Transfer Rates of Vertically Downward, Single
Plane Jet Air Curtains,IECEC Paper number: AIAA-2009-4610 11
Khalil, E.E., 1983, Modeling of Furnaces and Combustors, Abacus Press, UK. 12
Egyptian HVAC Code, HBRC, 2004