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Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering
          Research and Applications (IJERA)       ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue 4, July-August 2012, pp.1359-1363
      A Review On Exprimental & Numerical Investigation Of
                   Ranque Hilsch Vortextube
              Rahul B Patela , Dr. V. N. Bartariab , Tausif M Shaikhc


Abstract-
         The vortex tube or Ranque–Hilsch              inlet pressure and speed. Pressure difference occurs
vortex tube is a simple device used in industry        between tube wall and tube center because of the
for generation of cold and hot air streams from        friction of the fluid circling at high speeds. Speed
a single compressed air supply. This simple            of the fluid near the tube wall is lower than the
device is very efficient in separation of air          speed at the tube center, because of the effects of
streams of different temperatures and has been         wall friction. As a result, fluid in the center region
the focus of investigation since the tube’s            transfers energy to the fluid at the tube wall,
discovery. Different explanations for the              depending on the geometric structure of the vortex
phenomenon of the energy separation have been          tube. The cooled fluid leaves the vortex tube from
proposed, however there has not been a                 the cold output side, by moving towards an
consensus in the hypothesis. The purpose of this       opposite direction, compared to the main flow
paper is to present a critical review of current       direction, after a stagnation point. Whereas, the
explanations on the working concept of a vortex        heated fluid leaves the tube in the main flow
tube.                                                  direction from the other end (Dincer et al., in
Although many experimental and numerical               press). By injecting compressed air at room
studies on the vortex tubes have been made, the        temperature circumferentially into a tube at high
physical behaviour of the flow is not fully             velocity, a vortex tube can produce cold air down to
understood due to its complexity and the lack of       223 K and hot air up to 400 K (Crocker et al.,
consistency in the experimental findings.               2003).
Furthermore, several different hypotheses based
on experimental, analytical, and numerical
studies have been put forward to describe the
thermal separation phenomenon. Hypotheses of
pressure, viscosity, turbulence & temperature
separation phenomenon using CFD analysis of
vortex tube are discussed in the paper, and
presumably, future research will benefit from
this discussion.[1]
.
Index Terms—RHVT, Thermal Separation, CFD

I. INTRODUCTION
         Ranque discovered the effect of vortex
energy distribution and patented the first vortex
tube (RHVT) in 1934. In 1946, Hilsch improved
the RHVT design and its underlying principles that
still remain valid today (Khodorkov et al., 2003).
Aljuwayhel et al. (2005) define the vortex tube as a
simple device with no moving parts that is capable
of separating a high-pressure flow into two lower
pressure flows of different temperatures. The
device consists of a simple circular tube, one or
more tangential nozzles, and a throttle valve (see
Fig. 1, Cockerill, 1995).
Working principle of the counter flow RHVT can
be defined as follows. Compressible fluid, which is     Fig. 1 – Schematic diagram of the counter flow
tangentially introduced into the vortex tube from                   RHVT (Cockerill, 1995).
nozzles, starts to make a circular movement inside
the vortex tube at high speeds, because of the                Schematic diagram of the parallel flow
cylindrical structure of the tube, depending on its    RHVT is shown in Fig. 2. Both hot and cold flows


                                                                                             1359 | P a g e
Rahul B Patela, Dr. V. N. Bartariab ,Tausif M Shaikhc / International Journal of Engineering
          Research and Applications (IJERA)         ISSN: 2248-9622 www.ijera.com
                             Vol. 2, Issue 4, July-August 2012, pp.
in RHVTs leave the vortex tube in the same                on which physics can be applied for getting the
direction. It is not possible for cold flow to turn       results. The CFD software gives one the power to
back after a stagnation point. In order to separate       model things, mesh them, give proper boundary
the flow in the center of the tube from the flow at       conditions and simulate them with real world
the wall, an apparatus which has a hole in the            condition to obtain results. Using CFD a model can
center is used. The temperature of hot and cold           be developed which can breed to give results such
flows can be changed by back and forth movement           that the model could be developed into an object
of this apparatus. In parallel flow RHVTs, hot and        which could be of some use in our life.
cold flows mix with each other. This mixing affects
the temperatures of fluids negatively and causes          Modeling is the mathematical physics problem
their efficiencies to be low. For this reason, parallel   formulation in terms of a continuous initial
flow RHVTs are generally not preferred (Dincer,           boundary value problem (IBVP)
2005; Dincer et al., 2005)                                IBVP is in the form of Partial Differential
                                                          Equations (PDEs) with appropriate boundary
                                                          conditions and initial conditions.
                                                          Modeling includes:
                                                          1. Geometry and domain
                                                          2. Coordinates
                                                          3. Governing equations
                                                          4. Flow conditions
                                                          5. Initial and boundary conditions
                                                           6. Selection of models for different applications
                                                          Solve the Navier-Stokes equations (3D in Cartesian
                                                          coordinates) .
 Fig. 2 – Schematic diagram of the parallel flow
           RHVT (Dincer et al., 2005).                             Computational fluid dynamics techniques
                                                          have revolutionized engineering design in several
          In the conventional vortex tube,                important areas, notably in analysis of fluid flow
compressed gas enters directly a circular flow            technology. CFD can also be used as a minimal
passage with equal section area from a straight           adequate tool for design of engineering
pipe, which can cause a sudden change of flow             components. A careful scanning of various
direction at the joint between the straight pipe and      numerical investigations on the mechanism of
the circular flow passage. The sudden change              thermal separation in vortex tubes indicate that
would lead to the generation of eddies, which cause       barring a few ,no serious attempts have been made
energy loss. The sudden change of flow velocity           to use CFD techniques to simulate the flow patterns
and the eddy generated by this change can also            of vortex tubes.
cause the energy loss. It is important to have a high
peripheral velocity in the portion of the tube                     A detailed analysis of various parameters
immediately after the nozzle; the curve of the            of the vortex tube has been carried out through
nozzle affects the performance of vortex tubes (Wu        CFD techniques to simulate the phenomenon of
et al., 2007).                                            flow pattern, thermal separation, pressure gradient
RHVTs are used, among others, for cooling,                etc. so that they are comparable with the
heating, drying and snow production. Their cooling        experimental results.
capability is used, e.g., in dehumidifying gas
samples, chilling of environmental chambers,                        The vortex tube was first observed by
cooling of food, welding, and air climate control         Ranque. Later, Hilsch did some experimental and
processes. Although, they are not very efficient as a     theoretical studies to increase the efficiency of the
cooling device, they can be very useful in certain        vortex tube. Fulton explained the energy separation.
applications as they are small, simple to make and        He proposed that the inner layer heat the outer layer
repair, and require no electrical or chemical power       meanwhile expanding and growing cold. Reynolds
source. Nowadays, RHVTs are produced by                   did the numerical analysis of vortex tube. Lewellen
different commercial companies with a wide range          arrived at the solution by combining the three
of applications (Dincer et al., 2008). [2]                Navier-stokes equations for an incompressible fluid
                                                          in a strong rotating axisymmetric flow with a radial
II. INTRODUCTION                      TO         CFD      sink flow. Linderstorm-lang examined the velocity
MODELLING                                                 and thermal fields in the tube. He calculated the
         CFD is concerned with numerical solution         axial and radial gradients of the tangential velocity
of differential equations governing transport of          profile from prescribed secondary flow functions
mass, momentum and energy in moving fluid.                on the basis of a zero-order approximation to the
Using CFD, one can build a computational model

                                                                                               1360 | P a g e
Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering
          Research and Applications (IJERA)       ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue 4, July-August 2012, pp.1359-1363
momentum equations developed by Lewellen for an          parameters for obtaining the maximum hot gas
incompressible flow.                                     temperature and minimum cold gas temperature are
                                                         obtained through CFD analysis and validated
          Schlenz investigated numerically in a uni-     through experiments. The coefficient of
flow vortex tube, the flow field and the process of      performance (COP) of the vortex tube as a heat
energy separation. Calculations were carried out         engine and as a refrigerator has been calculated.
assuming a 2D axisymmetric compressible flow
and using the Galerkin's approach with a zero-                     Ahmet Murat Pinar et al, [6] were carried
equation turbulence model to solve the mass,             out Optimization of counter flow Ranque–Hilsch
momentum, and energy conservation equations to           vortex tube performance using Taguchi method.
calculate the flow and thermal fields. Amitani used      This study discusses the application of Taguchi
the mass, momentum and energy conservation               method in assessing maximum temperature
equation in a 2D model of a counter flow vortex          gradient for the Ranque–Hilsch counter flow vortex
tube with a short length, with an assumption of a        tube performance. The experiments were planned
helical motion in an axial direction for an invicid      based on Taguchi’s L27 orthogonal array with each
compressible perfect fluid. Flohlingsdorf and Unger      trial performed under different conditions of inlet
used the CFX system with the k-ϵ model to study          pressure, nozzle number and fluid type. Signal-to-
the velocity profile and energy separation in a          noise ratio (S/N) analysis, analysis of variance
vortex tube. Aljuwahel reported that RNG k-ϵ is          (ANOVA) and regression analysis were carried out
better than k-ϵ when he studied the energy               in order to determine the effects of process
separation and the flow phenomenon in a counter          parameters and optimal factor settings. Finally,
flow vortex tube using CFD in Fluent. T. Farouk          confirmation tests verified that Taguchi method
and B. Farouk introduced the large eddy simulation       achieved optimization of counter flow Ranque–
(LES) technique to predict the flow fields and the       Hilsch vortex tube performance with sufficient
associated temperature separation within a counter-      accuracy.
flow vortex tube for several cold mass fractions.
However, most of the computations found in the                     Tanvir Farouk et al, [7] carried out
literature used simple or the first-order turbulence     Simulation of gas species and temperature
models which are considered unsuitable for               separation in the counter-flow Ranque–Hilsch
complex, compressible vortex tube flows. The             vortex tube using the large eddy simulation
present work presents a two-dimensional numerical        technique.A computational fluid dynamic model is
investigation of flow and temperature separation         used to predict the species and temperature
behaviours inside a flow vortex tube.[3]                 separation within a counter flow Ranque–Hilsch
                                                         vortex tube. The large eddy simulation (LES)
III. EXPRIMENTAL & NUMRICAL                              technique was employed for predicting the gas flow
ANALYSIS                                                 and temperature fields and the species mass
          From 1934, almost 200-215 articles are         fractions (nitrogen and helium) in the vortex tube.
published on Ranque Hilsch vortex tube. Not all the      A vortex tube with a circumferential inlet stream of
articles are directly related to our work, especially,   nitrogen–helium mixture and an axial (cold) outlet
those articles which were focused on computational       stream and a circumferential (hot) outlet stream
work. Many articles addressed experimental               was considered. The temporal evolutions of the
findings and remaining discussed various theories        axial, radial and azimuthal components of the
explaining energy separation phenomenon. In this         velocity along with the temperature, pressure and
subsection, we are going to discuss only those           mass density and species concentration fields
articles (experimental and/or theoretical work)          within the vortex tube are simulated. Even though a
which are directly related to current work.[4]           large temperature separation was observed, only a
                                                         very minimal gas separation occurred due to
         Upendra Behera et al, [5] were carried out      diffusion effects. Correlations between the
CFD analysis and experimental investigations             fluctuating components of velocity, temperature
towards optimizing the parameters of Ranque–             and species mass fraction were calculated to
Hilsch vortex tube. Computational fluid dynamics         understand the separation mechanism. The inner
(CFD) and experimental studies are conducted             core flow was found to have large values of eddy
towards the optimization of the Ranque–Hilsch            heat flux and Reynolds’s stresses. Simulations were
vortex tubes. Different types of nozzle profiles and     carried out for varying amounts of cold outlet mass
number of nozzles are evaluated by CFD analysis.         flow rates. Performance curves (temperature
The swirl velocity, axial velocity and radial            separation/gas separation versus cold outlet mass
velocity components as well as the flow patterns         fraction) were obtained for a specific vortex tube
including secondary circulation flow have been           with a given inlet mass flow rate.
evaluated. The optimum cold end diameter (dc) and
the length to diameter (L/D) ratios and optimum

                                                                                              1361 | P a g e
Rahul B Patela, Dr. V. N. Bartariab ,Tausif M Shaikhc / International Journal of Engineering
          Research and Applications (IJERA)         ISSN: 2248-9622 www.ijera.com
                             Vol. 2, Issue 4, July-August 2012, pp.




     Fig. 1. Time averaged total temperature
  contours for the vortex tube in the r–x plane
(case 1). Time averaging was performed between
                   0.4 and 0.8 s




                                                          Fig. 1. Schematic diagram of a counter-flow
                                                                   Ranque–Hilsch vortex tube.

                                                        K. Dincer et al, [9] were carried out Experimental
   Fig. 2. Time averaged helium mass fraction           investigation of performance of hot cascade type
  contours for the vortex tube in the r–x plane         Ranque-Hilsch vortex tube and exergy analysis. In
(case 1). Time averaging was performed between          this study, three Ranque-Hilsch vortex tubes were
                  0.4 and 0.8 s.                        used, which have 9 mm inside diameter and
                                                        length/diameter ratio was 15. Their performances
          S. Eiamsa-ard [8] was carried out             were examined as one of the classical RHVT and
Experimental investigation of energy separation in      other was hot cascade type RHVT. Performance
a counter-flow Ranque–Hilsch vortex tube with           analysis was according to temperature difference
multiple inlet snail entries. The energy/               between the hot outlet and the inlet (ΔThot). The
Temperature separation phenomenon and cooling           ΔThot values of hot cascade type Ranque-Hilsch
efficiency characteristics in a counter-flow            vortex tubes were greater than the ΔThot values of
Ranque–Hilsch vortex tube (RHVT) are                    classical RHVT, which were determined
experimentally studied. The ascertainment focuses       experimentally. The total inlet exergy, total outlet
on the effects of the multiple inlet snail entries      exergy, total lost exergy and exergy efficiency of
(N=1 to 4 nozzles), cold orifice diameter ratios        hot stream were investigated by using experimental
(d/D=0.3 to 0.7) and inlet pressures (Pi=2.0 and 3.0    data. In both the classical RHVT and hot cascade
bar). The experiments using the conventional            type RHVT, it was found that as fraction of cold
tangential nozzles (N=4), are also performed for        flow increases the total lost exergy decreases. It
comparison. The experimental results reveal that        was also found that, the hot cascade type RHVT
the RHVT with the snail entry provides greater cold     more exergy efficiency of hot outlet than the
air temperature reduction and cooling efficiency        classical RHVT. Excess ΔThot value of hot cascade
than those offered by the RHVT with the                 type Ranque-Hilsch vortex tube causes the excess
conventional tangential inlet nozzle under the same     exergy efficiency of hot outlet.
cold mass fraction and supply inlet pressure. The
increase in the nozzle number and the supply                    H.M. Skye et al, [10] were carried out
pressure leads to the rise of the swirl/vortex          Comparison of CFD analysis to empirical data in a
intensity and thus the energy separation in the tube.   Commercial vortex tube. This paper presents a
                                                        comparison between the performance predicted by
                                                        a computational fluid dynamic (CFD) model and

                                                                                             1362 | P a g e
Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering
          Research and Applications (IJERA)       ISSN: 2248-9622 www.ijera.com
                     Vol. 2, Issue 4, July-August 2012, pp.1359-1363
experimental measurements taken using a                   [2]   K. Dincer et al, were carried out
commercially available vortex tube. Specifically,               ―Experimental investigation of the
the measured exit temperatures into and out of the              performance of a Ranque–Hilsch Vortex
vortex tube are compared with the CFD model. The                tube with regard to a plug located at the
data and the model are both verified using global               hot outlet‖.
mass and energy balances. The CFD model is a              [3] Prof. R. K. Sahoo et al, were carried out
two-dimensional (2D) steady axisymmetric model                  ―Numerical Analysis in Ranque-Hilsch
(with swirl) that utilizes both the standard and                Vortex tube.‖
renormalization group (RNG) k-epsilon turbulence          [4] Sachin U. Nimbalkar et al, were carried
models. While CFD has been used previously to                   out ―Quantitative observations on multiple
understand the fluid behavior internal to the vortex            flow structures inside Ranque Hilsch
tube, it has not been applied as a predictive model             vortex tube.‖
of the vortex tube in order to develop a design tool      [5] Upendra Behera et al, were carried out
that can be used with confidence over a range of                ―CFD       analysis    and     experimental
operating conditions and geometries. The objective              investigations towards optimizing the
of this paper is the demonstration of the successful            parameters of Ranque–Hilsch vortex
use of CFD in this regard, thereby providing a                  tube.‖
powerful tool that can be used to optimize vortex         [6] Ahmet Murat Pinar et al, were carried out
tube design as well as assess its utility in the                ―Optimization of counter flow Ranque–
context of new applications.                                    Hilsch vortex tube performance using
                                                                Taguchi method.‖
                                                          [7] Tanvir Farouk et al, were carried out
                                                                ―Simulation of gas species and
                                                                temperature separation in the counter-flow
                                                                Ranque–Hilsch vortex tube using the large
                                                                eddy simulation technique.‖
                                                          [8]. S.Eiamsa-ard         was      carried    out
                                                                ―Experimental investigation of energy
                                                                separation in a Counter- flow Ranque–
                                                                Hilsch vortex tube with multiple inlet snail
                                                                entries.‖
        Fig. 3. Picture of vortex tube used for           [9] .K. Dincer et al, were carried out
                      experiment.                               ―Experimental         investigation      of
                                                                performance of hot cascade type Ranque-
IV. CONCLUSION:-                                                Hilsch vortex tube and exergy analysis.‖
          The issue concerned in all explanations is      [10]. H.M. Skye et al, were carried out
the energy transfer between different layers. When              Comparison of CFD analysis to empirical
little energy is transferred from the inner flow to             data in a Commercial vortex tube.
the outer flow, the temperature drop of cold air can
be considered to be the result of sudden expansion
near the entrance, and the temperature rise of hot
air might be the result of friction of the multi-
circulation near the hot exit. Therefore, clarification
of the energy transfer between different layers is a
useful approach in the investigation of the vortex
tube. Clear understanding of the flow structure
inside the vortex tube is required for further
investigation, especially the region near the
entrance in which sudden expansion is considered
as the governing process and the region near the
exit in which multi-circulation may be formed.

From the above study I am much more interested to
work on Experimental & Numerical investigation
of Ranque-Hilsch vortex tube using CFD.

V. REFERENCES
  [1]     Yunpeng Xue et al, were carried out ―A
          critical review of temperature separation
          in a vortex tube‖.

                                                                                            1363 | P a g e

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Hr2413591363

  • 1. Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue 4, July-August 2012, pp.1359-1363 A Review On Exprimental & Numerical Investigation Of Ranque Hilsch Vortextube Rahul B Patela , Dr. V. N. Bartariab , Tausif M Shaikhc Abstract- The vortex tube or Ranque–Hilsch inlet pressure and speed. Pressure difference occurs vortex tube is a simple device used in industry between tube wall and tube center because of the for generation of cold and hot air streams from friction of the fluid circling at high speeds. Speed a single compressed air supply. This simple of the fluid near the tube wall is lower than the device is very efficient in separation of air speed at the tube center, because of the effects of streams of different temperatures and has been wall friction. As a result, fluid in the center region the focus of investigation since the tube’s transfers energy to the fluid at the tube wall, discovery. Different explanations for the depending on the geometric structure of the vortex phenomenon of the energy separation have been tube. The cooled fluid leaves the vortex tube from proposed, however there has not been a the cold output side, by moving towards an consensus in the hypothesis. The purpose of this opposite direction, compared to the main flow paper is to present a critical review of current direction, after a stagnation point. Whereas, the explanations on the working concept of a vortex heated fluid leaves the tube in the main flow tube. direction from the other end (Dincer et al., in Although many experimental and numerical press). By injecting compressed air at room studies on the vortex tubes have been made, the temperature circumferentially into a tube at high physical behaviour of the flow is not fully velocity, a vortex tube can produce cold air down to understood due to its complexity and the lack of 223 K and hot air up to 400 K (Crocker et al., consistency in the experimental findings. 2003). Furthermore, several different hypotheses based on experimental, analytical, and numerical studies have been put forward to describe the thermal separation phenomenon. Hypotheses of pressure, viscosity, turbulence & temperature separation phenomenon using CFD analysis of vortex tube are discussed in the paper, and presumably, future research will benefit from this discussion.[1] . Index Terms—RHVT, Thermal Separation, CFD I. INTRODUCTION Ranque discovered the effect of vortex energy distribution and patented the first vortex tube (RHVT) in 1934. In 1946, Hilsch improved the RHVT design and its underlying principles that still remain valid today (Khodorkov et al., 2003). Aljuwayhel et al. (2005) define the vortex tube as a simple device with no moving parts that is capable of separating a high-pressure flow into two lower pressure flows of different temperatures. The device consists of a simple circular tube, one or more tangential nozzles, and a throttle valve (see Fig. 1, Cockerill, 1995). Working principle of the counter flow RHVT can be defined as follows. Compressible fluid, which is Fig. 1 – Schematic diagram of the counter flow tangentially introduced into the vortex tube from RHVT (Cockerill, 1995). nozzles, starts to make a circular movement inside the vortex tube at high speeds, because of the Schematic diagram of the parallel flow cylindrical structure of the tube, depending on its RHVT is shown in Fig. 2. Both hot and cold flows 1359 | P a g e
  • 2. Rahul B Patela, Dr. V. N. Bartariab ,Tausif M Shaikhc / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue 4, July-August 2012, pp. in RHVTs leave the vortex tube in the same on which physics can be applied for getting the direction. It is not possible for cold flow to turn results. The CFD software gives one the power to back after a stagnation point. In order to separate model things, mesh them, give proper boundary the flow in the center of the tube from the flow at conditions and simulate them with real world the wall, an apparatus which has a hole in the condition to obtain results. Using CFD a model can center is used. The temperature of hot and cold be developed which can breed to give results such flows can be changed by back and forth movement that the model could be developed into an object of this apparatus. In parallel flow RHVTs, hot and which could be of some use in our life. cold flows mix with each other. This mixing affects the temperatures of fluids negatively and causes Modeling is the mathematical physics problem their efficiencies to be low. For this reason, parallel formulation in terms of a continuous initial flow RHVTs are generally not preferred (Dincer, boundary value problem (IBVP) 2005; Dincer et al., 2005) IBVP is in the form of Partial Differential Equations (PDEs) with appropriate boundary conditions and initial conditions. Modeling includes: 1. Geometry and domain 2. Coordinates 3. Governing equations 4. Flow conditions 5. Initial and boundary conditions 6. Selection of models for different applications Solve the Navier-Stokes equations (3D in Cartesian coordinates) . Fig. 2 – Schematic diagram of the parallel flow RHVT (Dincer et al., 2005). Computational fluid dynamics techniques have revolutionized engineering design in several In the conventional vortex tube, important areas, notably in analysis of fluid flow compressed gas enters directly a circular flow technology. CFD can also be used as a minimal passage with equal section area from a straight adequate tool for design of engineering pipe, which can cause a sudden change of flow components. A careful scanning of various direction at the joint between the straight pipe and numerical investigations on the mechanism of the circular flow passage. The sudden change thermal separation in vortex tubes indicate that would lead to the generation of eddies, which cause barring a few ,no serious attempts have been made energy loss. The sudden change of flow velocity to use CFD techniques to simulate the flow patterns and the eddy generated by this change can also of vortex tubes. cause the energy loss. It is important to have a high peripheral velocity in the portion of the tube A detailed analysis of various parameters immediately after the nozzle; the curve of the of the vortex tube has been carried out through nozzle affects the performance of vortex tubes (Wu CFD techniques to simulate the phenomenon of et al., 2007). flow pattern, thermal separation, pressure gradient RHVTs are used, among others, for cooling, etc. so that they are comparable with the heating, drying and snow production. Their cooling experimental results. capability is used, e.g., in dehumidifying gas samples, chilling of environmental chambers, The vortex tube was first observed by cooling of food, welding, and air climate control Ranque. Later, Hilsch did some experimental and processes. Although, they are not very efficient as a theoretical studies to increase the efficiency of the cooling device, they can be very useful in certain vortex tube. Fulton explained the energy separation. applications as they are small, simple to make and He proposed that the inner layer heat the outer layer repair, and require no electrical or chemical power meanwhile expanding and growing cold. Reynolds source. Nowadays, RHVTs are produced by did the numerical analysis of vortex tube. Lewellen different commercial companies with a wide range arrived at the solution by combining the three of applications (Dincer et al., 2008). [2] Navier-stokes equations for an incompressible fluid in a strong rotating axisymmetric flow with a radial II. INTRODUCTION TO CFD sink flow. Linderstorm-lang examined the velocity MODELLING and thermal fields in the tube. He calculated the CFD is concerned with numerical solution axial and radial gradients of the tangential velocity of differential equations governing transport of profile from prescribed secondary flow functions mass, momentum and energy in moving fluid. on the basis of a zero-order approximation to the Using CFD, one can build a computational model 1360 | P a g e
  • 3. Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue 4, July-August 2012, pp.1359-1363 momentum equations developed by Lewellen for an parameters for obtaining the maximum hot gas incompressible flow. temperature and minimum cold gas temperature are obtained through CFD analysis and validated Schlenz investigated numerically in a uni- through experiments. The coefficient of flow vortex tube, the flow field and the process of performance (COP) of the vortex tube as a heat energy separation. Calculations were carried out engine and as a refrigerator has been calculated. assuming a 2D axisymmetric compressible flow and using the Galerkin's approach with a zero- Ahmet Murat Pinar et al, [6] were carried equation turbulence model to solve the mass, out Optimization of counter flow Ranque–Hilsch momentum, and energy conservation equations to vortex tube performance using Taguchi method. calculate the flow and thermal fields. Amitani used This study discusses the application of Taguchi the mass, momentum and energy conservation method in assessing maximum temperature equation in a 2D model of a counter flow vortex gradient for the Ranque–Hilsch counter flow vortex tube with a short length, with an assumption of a tube performance. The experiments were planned helical motion in an axial direction for an invicid based on Taguchi’s L27 orthogonal array with each compressible perfect fluid. Flohlingsdorf and Unger trial performed under different conditions of inlet used the CFX system with the k-ϵ model to study pressure, nozzle number and fluid type. Signal-to- the velocity profile and energy separation in a noise ratio (S/N) analysis, analysis of variance vortex tube. Aljuwahel reported that RNG k-ϵ is (ANOVA) and regression analysis were carried out better than k-ϵ when he studied the energy in order to determine the effects of process separation and the flow phenomenon in a counter parameters and optimal factor settings. Finally, flow vortex tube using CFD in Fluent. T. Farouk confirmation tests verified that Taguchi method and B. Farouk introduced the large eddy simulation achieved optimization of counter flow Ranque– (LES) technique to predict the flow fields and the Hilsch vortex tube performance with sufficient associated temperature separation within a counter- accuracy. flow vortex tube for several cold mass fractions. However, most of the computations found in the Tanvir Farouk et al, [7] carried out literature used simple or the first-order turbulence Simulation of gas species and temperature models which are considered unsuitable for separation in the counter-flow Ranque–Hilsch complex, compressible vortex tube flows. The vortex tube using the large eddy simulation present work presents a two-dimensional numerical technique.A computational fluid dynamic model is investigation of flow and temperature separation used to predict the species and temperature behaviours inside a flow vortex tube.[3] separation within a counter flow Ranque–Hilsch vortex tube. The large eddy simulation (LES) III. EXPRIMENTAL & NUMRICAL technique was employed for predicting the gas flow ANALYSIS and temperature fields and the species mass From 1934, almost 200-215 articles are fractions (nitrogen and helium) in the vortex tube. published on Ranque Hilsch vortex tube. Not all the A vortex tube with a circumferential inlet stream of articles are directly related to our work, especially, nitrogen–helium mixture and an axial (cold) outlet those articles which were focused on computational stream and a circumferential (hot) outlet stream work. Many articles addressed experimental was considered. The temporal evolutions of the findings and remaining discussed various theories axial, radial and azimuthal components of the explaining energy separation phenomenon. In this velocity along with the temperature, pressure and subsection, we are going to discuss only those mass density and species concentration fields articles (experimental and/or theoretical work) within the vortex tube are simulated. Even though a which are directly related to current work.[4] large temperature separation was observed, only a very minimal gas separation occurred due to Upendra Behera et al, [5] were carried out diffusion effects. Correlations between the CFD analysis and experimental investigations fluctuating components of velocity, temperature towards optimizing the parameters of Ranque– and species mass fraction were calculated to Hilsch vortex tube. Computational fluid dynamics understand the separation mechanism. The inner (CFD) and experimental studies are conducted core flow was found to have large values of eddy towards the optimization of the Ranque–Hilsch heat flux and Reynolds’s stresses. Simulations were vortex tubes. Different types of nozzle profiles and carried out for varying amounts of cold outlet mass number of nozzles are evaluated by CFD analysis. flow rates. Performance curves (temperature The swirl velocity, axial velocity and radial separation/gas separation versus cold outlet mass velocity components as well as the flow patterns fraction) were obtained for a specific vortex tube including secondary circulation flow have been with a given inlet mass flow rate. evaluated. The optimum cold end diameter (dc) and the length to diameter (L/D) ratios and optimum 1361 | P a g e
  • 4. Rahul B Patela, Dr. V. N. Bartariab ,Tausif M Shaikhc / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue 4, July-August 2012, pp. Fig. 1. Time averaged total temperature contours for the vortex tube in the r–x plane (case 1). Time averaging was performed between 0.4 and 0.8 s Fig. 1. Schematic diagram of a counter-flow Ranque–Hilsch vortex tube. K. Dincer et al, [9] were carried out Experimental Fig. 2. Time averaged helium mass fraction investigation of performance of hot cascade type contours for the vortex tube in the r–x plane Ranque-Hilsch vortex tube and exergy analysis. In (case 1). Time averaging was performed between this study, three Ranque-Hilsch vortex tubes were 0.4 and 0.8 s. used, which have 9 mm inside diameter and length/diameter ratio was 15. Their performances S. Eiamsa-ard [8] was carried out were examined as one of the classical RHVT and Experimental investigation of energy separation in other was hot cascade type RHVT. Performance a counter-flow Ranque–Hilsch vortex tube with analysis was according to temperature difference multiple inlet snail entries. The energy/ between the hot outlet and the inlet (ΔThot). The Temperature separation phenomenon and cooling ΔThot values of hot cascade type Ranque-Hilsch efficiency characteristics in a counter-flow vortex tubes were greater than the ΔThot values of Ranque–Hilsch vortex tube (RHVT) are classical RHVT, which were determined experimentally studied. The ascertainment focuses experimentally. The total inlet exergy, total outlet on the effects of the multiple inlet snail entries exergy, total lost exergy and exergy efficiency of (N=1 to 4 nozzles), cold orifice diameter ratios hot stream were investigated by using experimental (d/D=0.3 to 0.7) and inlet pressures (Pi=2.0 and 3.0 data. In both the classical RHVT and hot cascade bar). The experiments using the conventional type RHVT, it was found that as fraction of cold tangential nozzles (N=4), are also performed for flow increases the total lost exergy decreases. It comparison. The experimental results reveal that was also found that, the hot cascade type RHVT the RHVT with the snail entry provides greater cold more exergy efficiency of hot outlet than the air temperature reduction and cooling efficiency classical RHVT. Excess ΔThot value of hot cascade than those offered by the RHVT with the type Ranque-Hilsch vortex tube causes the excess conventional tangential inlet nozzle under the same exergy efficiency of hot outlet. cold mass fraction and supply inlet pressure. The increase in the nozzle number and the supply H.M. Skye et al, [10] were carried out pressure leads to the rise of the swirl/vortex Comparison of CFD analysis to empirical data in a intensity and thus the energy separation in the tube. Commercial vortex tube. This paper presents a comparison between the performance predicted by a computational fluid dynamic (CFD) model and 1362 | P a g e
  • 5. Rahul B Patel, Dr. V. N. Bartaria , Tausif M Shaikh / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 2, Issue 4, July-August 2012, pp.1359-1363 experimental measurements taken using a [2] K. Dincer et al, were carried out commercially available vortex tube. Specifically, ―Experimental investigation of the the measured exit temperatures into and out of the performance of a Ranque–Hilsch Vortex vortex tube are compared with the CFD model. The tube with regard to a plug located at the data and the model are both verified using global hot outlet‖. mass and energy balances. The CFD model is a [3] Prof. R. K. Sahoo et al, were carried out two-dimensional (2D) steady axisymmetric model ―Numerical Analysis in Ranque-Hilsch (with swirl) that utilizes both the standard and Vortex tube.‖ renormalization group (RNG) k-epsilon turbulence [4] Sachin U. Nimbalkar et al, were carried models. While CFD has been used previously to out ―Quantitative observations on multiple understand the fluid behavior internal to the vortex flow structures inside Ranque Hilsch tube, it has not been applied as a predictive model vortex tube.‖ of the vortex tube in order to develop a design tool [5] Upendra Behera et al, were carried out that can be used with confidence over a range of ―CFD analysis and experimental operating conditions and geometries. The objective investigations towards optimizing the of this paper is the demonstration of the successful parameters of Ranque–Hilsch vortex use of CFD in this regard, thereby providing a tube.‖ powerful tool that can be used to optimize vortex [6] Ahmet Murat Pinar et al, were carried out tube design as well as assess its utility in the ―Optimization of counter flow Ranque– context of new applications. Hilsch vortex tube performance using Taguchi method.‖ [7] Tanvir Farouk et al, were carried out ―Simulation of gas species and temperature separation in the counter-flow Ranque–Hilsch vortex tube using the large eddy simulation technique.‖ [8]. S.Eiamsa-ard was carried out ―Experimental investigation of energy separation in a Counter- flow Ranque– Hilsch vortex tube with multiple inlet snail entries.‖ Fig. 3. Picture of vortex tube used for [9] .K. Dincer et al, were carried out experiment. ―Experimental investigation of performance of hot cascade type Ranque- IV. CONCLUSION:- Hilsch vortex tube and exergy analysis.‖ The issue concerned in all explanations is [10]. H.M. Skye et al, were carried out the energy transfer between different layers. When Comparison of CFD analysis to empirical little energy is transferred from the inner flow to data in a Commercial vortex tube. the outer flow, the temperature drop of cold air can be considered to be the result of sudden expansion near the entrance, and the temperature rise of hot air might be the result of friction of the multi- circulation near the hot exit. Therefore, clarification of the energy transfer between different layers is a useful approach in the investigation of the vortex tube. Clear understanding of the flow structure inside the vortex tube is required for further investigation, especially the region near the entrance in which sudden expansion is considered as the governing process and the region near the exit in which multi-circulation may be formed. From the above study I am much more interested to work on Experimental & Numerical investigation of Ranque-Hilsch vortex tube using CFD. V. REFERENCES [1] Yunpeng Xue et al, were carried out ―A critical review of temperature separation in a vortex tube‖. 1363 | P a g e