Experimental Study of Augmentation Technique for Turbulent Flow through Circular Pipe using Different Blockages

DOI : 10.17577/IJERTV3IS051079

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Experimental Study of Augmentation Technique for Turbulent Flow through Circular Pipe using Different Blockages

Shivaji V. Mundhe1

Applied Science dept., PICT, Pune Pune, India

Abstract – High performance heat transfer system is of great importance in many industrial applications. The performance of conventional heat exchangers can be substantially improved by a number of heat transfer enhancement techniques. A variety of complex, highly viscous liquids are involved that undergoes heat exchange process while flowing through heat exchangers. Because of their viscous nature, they tend to have low flow rates and generally represent the dominant thermal resistance due to their viscous nature, adversely affecting size and cost of heat exchanger. The process industry is continuously working to incorporate enhancement in heat transfer. Enhancement techniques can be classified as active methods, which require external power or Passive methods, which require no direct application of external power. The enhanced surfaces are routinely used to improve thermal and hydraulic performance of heat

Prashant W. Deshmukp Applied Science dept., PICT, Pune Pune, India

enhancement in heat transfer. Enhancement techniques can be classified as active methods which require external power and passive methods, which require no direct application of external power. The enhanced surfaces are routinely used to improve thermal and hydraulic performance of heat exchangers. These heat exchangers are used in process industries, air-conditioning, refrigeration, power generation etc. Secondary flows are created by these techniques, causing the separation of the boundary layer results in better bulk fluid mixing which reduces the temperature gradients in the fluid flow.

It is expected that a heat transfer augmentation device should produce significant increase in heat transfer. There are many performance evaluation criteria available in the literature. In the present analysis, the performance evaluation criteria R1 at constant flow rate (at same Reynolds number Re) is used to compare the performance of different cases.

exchangers. Experimental investigation of heat transfer of

circular tube fitted with helical wire and twisted tape, have been studied under uniform heat flux conditions. Air is

The performance criterion, defined as:

R1 at equal pumping power is

used as working fluid. The analysis is carried out for fully

developed turbulent flow having Reynolds number range based on test tube inside diameter from 5,000 to 20,000.

R1

Nu

Nuo

(1)

The experimental data obtained are compared with the

Nusslet number,

Nuo for turbulent flows are evaluated at the

smooth tube data available in the literature.

Keywords – Heat Transfer Enhancement, Augmentation,

same Reynolds number for smooth tube given by following Dittus Boelter Correlation.

o

Turbulent Flow, Inserts, Passive Method

  1. INTRODUCTION

    Nu 0.023Re0.8 Pr0.4

    (2)

    High performance heat transfer system is of great importance in many industrial applications. The performance of conventional heat exchangers can be substantially improved by a number of heat transfer enhancement techniques. A variety of complex, highly viscous liquids are involved that undergoes heat exchange process while flowing through heat exchangers. Because of their viscous nature, they tend to have low flow rates and generally represent the dominant thermal resistance due to their viscous nature, adversely affecting size and cost of heat exchanger. The process industry is continuously working to incorporate

  2. EXPERIMENTAL SET UP, DATA REDUCTION AND

    VALIDATION

    The experimental set up used for measuring Nusselt number is described. The details of the experimental set up, data reduction and validation are presented. The experimental procedure followed to obtain the heat transfer is discussed. Heat transfer results for turbulent flow in the smooth tube are compared with the correlations of Dittus Boelter.

    1. Experimental Set-up

      An experimental test facility to measure heat transfer for smooth tube and other inserts, is constructed. Figure 3.1 shows the schematic arrangement of the experimental setup used. The test section is 1000 mm long stainless steel tube of wall thickness 5 mm and an outside diameter of do equal to

      35.4 mm. In order to ensure the hydro-dynamically fully

      developed flow, a pipe of length 40 times the pipe diameter is provided upstream to the test section. Nine calibrated Chromel-Alumel K-type thermocouples 100 mm axially apart are placed over the tube. To provide uniform heat flux, an electrical resistance coil is wrapped around the circumference of entire test section form inlet to the outlet. The test section is

      w

      thermally insulated using ceramic wool to minimise the heat loss.

      As the flow of air is single phase, it is assumed that the bulk temperature is linearly varying across the test section from inlet to outlet. The intermediate values are obtained by interpolation between inlet and outlet bulk temperatures. The value of Nusselt number for fully developed flow is determined as:

      Qout d

      Nuavg AT

      x Tb xk

      (6)

      The Nusselt number for smooth tube is obtained by using Dittus-Boelter Equation.

      NuS

      0.023 Re0.8 Pr0.4

      (7)

      Fig 1. Schematic of Experimental Set up

      Air as working fluid is forced into test section using an air blower. The flow rate of air in test section is regulated using an inlet valve and a by-pass valve. The mass flow rate is calculated by anemometer. The Reynolds number, Re based on the tube inner diameter is varied from 4000 to 10000. A thermocouple is placed at entry and exit of the test section respectively to measure the bulk mean air temperature.

    2. Experimental Procedure

      Test fluid, air is allowed to flow through the test section. The mass flow rate of air is adjusted by the valve so that it will give the required Reynolds number at the test section. The entire periphery of the test section is provided with constant uniform heat flux through variable transformer. The input power to the test section is adjusted such that the temperature difference between the mean wall temperature and mean bulk is around 15°C. The system is allowed to reach steady state for each reading of Reynolds number. The approximate time duration for the system to reach steady state is found to be 1.5 to 2.0 hours. At steady state, the temperature readings of wall, inlet and outlet are recorded. The value of Nusselt number is calculated for each wall thermocouple temperature readings. The wall temperature is taken at the thermocouple which is placed at L/d ratio more than 10. Nusselt number thus calculated is the mean of the Nusselt number obtained at various axial locations of the wall.

    3. Data Reduction

      The mass flow rate is calculated based on the velocity measurement using an anemometer.

      The total input power supplied to the test section is calculated from measurement of current and voltage supplied to it.

    4. Validation of the Experimental Test Set Up

    The experimental test facility is validated for heat transfer smooth tube flow. The data for smooth tube flow is available in the literature. Experimental data of Nusselt number for smooth tube flow at different Reynolds number, are validated using correlation of Dittus-Boelter. Figure 2. shows Nusselt number as a function of Reynolds number. There is a fairly ood agreement between the values predicted by Dittus- Boelter with the experimentally obtained values of Nusselt number.

    Fig 2. Variation of Nusselt number, Nu with Reynolds number, Re for smooth tube flow

    Fig 3. % Variation of Nusselt number, Nu with Reynolds number, Re for smooth tube flow

    Qin V I

    Heat carried by air from test section is

    Qout m CP Tbo Tbi

    (3)

    (4)

    Figure 3. shows that the present analysis has a variation of less than 8 % in the measurement of Nusselt number with values specified by Dittus Boelter Correlation.

  3. Results and Discussion

    Outlet and inlet temperature of air

    Tbo ,Tbi

    is measured

    The experimental data for heat transfer characteristics for

    using three thermocouples located at each end of the test section.

    The unaccounted heat shall not exceed 10% of the total heat supplied. Therefore, the energy balance is checked by following equation

    modified tube, helical wire coil is obtained. In this chapter, comparison of performance characteristics of different configuration of the tube is carried out. The parameters like percentage of blockage of the tube and Reynolds number Re, are systematically varied.

    Qin Qout 10%

    Qin

    (5)

    Test Sectio

    Central Rod

    2) Heat transfer results of Tests section with 10 mm diameter Rod

    Figure 7. show the variation of Nusselt number with Reynolds number for test section with 10 mm diameter central rod and for the smooth tube. It is observed that

    Fig. 4. Vortex generator in round tube

    The results are expressed in terms of % of enhancement over the corresponding smooth tube heat transfer.

    1. Technical Details of the tube

      The central core portion of the tube is blocked by a rod of three different diameters viz, 8 mm, 10 mm and 12 mm. Figure 4 shows the schematic of the tube. The rod is placed inside the tube in such a way that it remain exactly at the centre position of the test section

    2. Results and Discussion

      The experimental results are expressed in terms of Nusselt number ratios as a function of % of blockage and Reynolds Number Re. The ratio of Nusselt number for augmented case to the Nusselt number for smooth tube, at equal Reynolds numbers are presented as the performance ratio R1,. i.e. Nu/Nuo. at equal Reynolds number specified as Nu/Nuc..

      1. Heat transfer results of Tests section with 8 mm diameter Rod

    Fig 5. Variation of Nusselt number, Nu with Reynolds number, Re

    for Test section with 8 mm central Rod.

    Fig 6. Variation of Performance Ratio R1 i.e. Nu/Nuo with Reynolds number,

    Re for Tube with 8 mm central rod.

    Figure 5. show the variation of Nusselt number with Reynolds number for test section with 8 mm diameter central rod and for the smooth tube. It is observed that there is significantly rise in heat transfer enhancement of heat transfer. Figure 6. shows that the performance ratio R1 i.e. Nu/Nuo is found to be in the range of 1.2 to 1.4. i.e. % of enhancement is found to be 20% to 50% more in comparison with the smooth tube.

    Fig 8. Variation of Nusselt number, Nu with Reynolds number, Re

    for Test section with 10 mm central Rod.

    Fig 8. Variation of Performance Ratio R1 i.e. Nu/Nuo with Reynolds number, Re for Tube with 10 mm central rod.

    there is significantly rise in heat transfer enhancement of heat transfer. Figure 8. shows that the performance ratio R1 i.e. Nu/Nuo is found to be in the range of 1.4 to 1.6. i.e. % of enhancement is found to be 40% to 60% more in comparison with the smooth tube.

    1. Heat transfer results of Tests section with 12 mm diameter Rod

      Fig 9. Variation of Nusselt number, Nu with Reynolds number, Re

      for Test section with 12 mm central Rod.

      Fig 10. Variation of Performance Ratio R1 i.e. Nu/Nuo with Reynolds number, Re for Tube with 12 mm central rod.

      Figure 9. show the variation of Nusselt number with Reynolds number for test section with 12 mm diameter central rod and for the smooth tube. It is observed that there is significantly rise in heat transfer enhancement of heat transfer. Figure 10 shows that the performance ratio R1 i.e. Nu/Nuo is found to be in the range of 1.2 to 1.3. i.e. % of enhancement is found to be 20% to 30% more in comparison with the smooth tube.

    2. Comparison of Heat transfer results of Tests section with Different central Rods

      The comparison of the performance characteristics of all the three configuration of the tests section is shown in fig. 11. and 12. It is observed that the test section with 10 mm diameter rod gives maximum heat transfer in comparison with the test section having central rod of 8 mm and 12 mm. This is true for all the three values of Reynolds number

      Fig 11. Variation of Nusselt number, Nu with Reynolds number, Re

      for Three Different Configurations of Test section

      Fig 12. Variation of Performance Ratio R i.e. Nu/Nu with Reynolds number,

      Figure 13 and 14 shows that helical wire coil provides heat transfer around 2.0 to 3.7 times as that of the smooth tube. Hence it reveals that the helical wire coil is the best heat transfer enhancement technique in turbulent flows.

      The measurements of heat transfer in round tube are carried out to understand heat transfer performance of

      Fig 14. Variation of Performance Ratio R1 i.e. Nu/Nuo with Reynolds number, Re for Helical Wire Coil

      the test section having different percentage of blockages at its centre.

  4. CONCLUSIONS

The measurements of heat transfer in round tube are carried out to understand heat transfer performance of the test section having different percentage of blockages at its centre. Following are the conclusions that may be drawn from the experimental data obtained.

  • Experimental investigation of heat transfer of circular tube fitted with different percentages blockages, have been studied under uniform heat flux conditions with air as the working fluid.

  • All the three configurations show the Nusselt number augmentation (Nu/Nuo) of 1.2 to 1.5 for all the three Reynolds number studied.

  • This enhancement in heat transfer is due to division / breaking or separation of boundary layers. This causes reduction in temperature and velocity gradients in the flow,

    1 o results in enhancement of heat transfer.

    Re for Tube with 12 mm central rod.

    1. Investigation of Helical wire coil heat transfer performance

    Helical wire coils is considered as the best heat transfer enhancement device in round tubes as it breaks the laminar sub layer which is exists near the tube wall for turbulent flow. The configuration of helical wire coil (pitch to inner diameter ratio p/d = 1.18, wire diameter 2.5 mm) is analyzed in the present experimental set up.

    Fig 13. Variation of Nusselt number, Nu with Reynolds number, Re for Helical Wire Coil

  • One configuration of helical wire coil is tested and it is found that it is best heat transfer enhancement techniques giving Nusselt number augmentation in the range of 2.0 3.7. But at the same time it may increase the pressure drop across the tube

REFERENCES

  1. Manglik R. M. and Bergles A. E., Heat Transfer and pressure drop correlations for twisted tape inserts in isothermal tubes: Part I

    Laminar Flows, Journal of Heat Transfer, vol 115,(1993) 881- 889

  2. Liao Q. and Xin M.D., Augmentation of convective heat transfer inside tubes with three-dimensional internal extended surfaces and twisted-tape inserts, Chemical Engineering Journal, 78 (2000) 95 105

  3. Garca A., Vicente P.G., and Viedma A., Experimental study of heat transfer enhancement with wire coil inserts in laminar-transition- turbulent regimes at different Prandtl numbers, International Journal of Heat and Mass Transfer, 48 (2005) 46404651

  4. Eiamsa-rd S., Promvonge P., Enhancement of heat transfer in a tube with regularly-spaced helical tape swirl generators, Solar Energy, 78 (2005) 483494

  5. Sivashanmugam P. and Nagarajan P.K., Studies on heat transfer and friction factor characteristics of laminar flow through a circular tube

    fitted with right and left helical screw-tape inserts, Experimental Thermal and Fluid Science, 32 (2007) 192197

  6. Eiamsa-ard S., Rattanawong S., and Promvonge P., Turbulent convection in round tube equipped with propeller type swirl generators, International Communications in Heat and Mass Transfer, 36 (2009) 357364

  7. Eiamsa-ard S., Promvonge P., Performance assessment in a heat exchanger tube with alternate clockwise and counter-clockwise twisted-tape inserts, International Journal of Heat and Mass Transfer, 53 (2010) 13641372

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