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NUMERICAL SIMULATION OF FLOW AND HEAT TRANSFER IN A COOLING CHANNEL WITH STAGGERED V-SHAPED RIBS

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(1)

명 현 국,*1 김 광 용2

N UMERICAL S IMULATION OF F LOW AND H EAT T RANSFER IN A C OOLING C HANNEL WITH S TAGGERED V - S HAPED R IBS

H.K. Myong

*1

and K.Y. Kim

2

The present study numerically simulates the flow and heat transfer characteristics of rib-induced secondary flow in a square cooling channel with staggered V-shaped ribs, extruded on both walls. The rib pitch-to-height ratio (  ) varies from 2.8 to 10 with the rib-height-to-hydraulic diameter ration ( 

) of 0.07 and the Reynolds number of 50,000. Shear stress transport (SST) turbulence model is used as a turbulence model. Computational results show that complex secondary flow patterns are generated in the channel due to the snaking flow in the streamwise direction for all tested cases. In the range of  =5 to 10 the staggered V-shaped rib gives about 3 times higher heat transfer augmentation than the reference smooth pipe with high heat transfer on both front side and the area around the leading edge of the ribs, while the former cases give about 18 times higher streamwise pressure drop than the latter ones. However, for the thermal performances, based on the equal pumping power condition, the case of  =2.8 gives the best result among three cases, mainly due to relatively low streamwise pressure drop, although it gives relatively low heat transfer augmentation.

Key Words : V- (Staggered V-Shaped Rib), (Flow and Heat Transfer), (Numerical Simulation), (Cooling Channel)

* Corresponding author, E-mail: [email protected]

1.

(cooling channel) (rib), (pin fin), (dimple)

(turbulence promoter) .

, (vortex)

. ,

[1-5] . Han et

al.[1], Taslim et al.[2] Talsim and Wadsworth[4]

V-

. V-

RANS(Reynolds Averaged

Navier-Stokes equations) [6-8]

,

.

[1-9] 

0.05   

0.25 , 

 5   20

. Horiuchi et al.[10] LES

Fig. 1 V-

(staggered V-shape rib) V- (continuous

V-shaped rib)

(2)

Fig. 1 Schematic of the cooling duct with staggered V-shaped rib and the top view with location of specified sections

.   

,  

. ,

,

. Gee and Webb[11]

(pumping power)

  (thermal

performance)  .

Fig. 1

V- RANS

, V-

.

 

0.07,   50,000 , -

 2.8, 5.0 10

. V-

.

2.

2.1

(unstructured grid system)

Fluent[12] .

,

(Fig. 1 ).

.

 

 

  (1)

 



 

  

 

    

  

 

   



 

 



(2)

 

  

  

 

 

   



   

  

 

    



(3)

         

.

        (4)

         (5)

 , 

 ,

     

    



 (6)

(6) 



.

SST(Shear Stress Transport) [13] .

SST      

,    ,

   . SST

(flow separation)

[14] ,

.

2.2

V-

Fig. 1  

( ) , 

 

,  

50,000 . , Horiuchi

et al.[10]    

,

α=70° ,

(3)

(a)

 

2.8 (b)

 

5 (c)

 

10 Fig. 2 Velocity vectors at z=0 plane

(a)

 

2.8 (b)

 

5 (c)

 

10 Fig. 3 Velocity vectors at z=



plane

 2.8, 5.0 10 .

1 ,

(Fig. 1 ).

1

  .

 2.8, 5.0 10 8.6×10

5

, 6.4×10

5

1.0×10

6

.

, ,

,

(4)

(a)

 

2.8 (Section B-1) (b)  5 (Section B-1) (c)

 

10 (Section B-1)

(d)

 

2.8 (Section B-4) (e)

 

5 (Section B-4) (f)

 

10 (Section B-4) Fig. 4 Velocity vectors at Sections B-1 and B-4

.

3.

Fig. 2 Fig. 3  (z = 0 )

(z =   )

.

.

 10 (Fig. 2(c))

, 2 .

.

 ,

 5 (Fig. 2(b))

1.5 ,

.

=2.8 (Fig. 2(a))

V- ,

.

. , Fig. 3

.

,

, V-

.  10

(Fig. 3(c)) .

,

.

(5)

(a)

 

2.8 (b)

 

5 (c)

 

10 Fig. 6 Local Nusselt number distributions

(a)

 

2.8 (b)

 

5 (c)

 

10 Fig. 5 Velocity vectors at  0.25 plane

Fig. 4 B Section(Fig. 1 )

,

.

(snaking flow) .

,

.

.

=2.8 , Fig. 4(a) B-1 Section

, .

B-1 Section ,

(6)

   

=2.8

1.82 1.78 1.50

=5

3.16 18.13 1.20



=10

2.83 16.21 1.12

Table 1 Summary of heat transfer performance comparison with respect to  ratios for V-shape ribs

,

. ,

.

,  10 (Fig. 4(c)) . B-4 Section(Fig. 1 )

,

. =2.8 (Fig.

4(d))

.

, >5

.

 5 (Fig. 4(e)) .

Fig. 5 ( 0.25 )

. ,  5 (Fig.

5(b)) Fig. 2

.  2.8 (Fig.

5(a))

.  10 (Fig. 5(c))

.

Fig. 6 

. ,  2.8 (Fig. 6(a))

 ( ) ,

. ,  5 (Fig. 6(b))

.  10 (Fig. 6(c))

,

 5 .

Table 1

  Gee and Webb[11]

  

.

  

     





(7)

,  

, Dittus-Boelter .

V-

. ,  5 3

18 .

-

.

  

V-

.

 2.8 1.5

.

,

5   20

.

4.

V- RANS

, V-

(7)

.  

0.07,   

50,000 , -  2.8, 5.0

10 .

V-

. ,

(1) -

, V-

.

(2) V-

V-

. (3)

 2.8 ,

 10 .

2006

(No. R01-2006-000-10039-0) .

[1] 1991, Han, J.C., Zhang, Y.M. and Lee, C.P., "Augmented Heat Transfer in Square Channels with Parallel, Crossed, and V shaped Angled Ribs," Journal of Heat Transfer, Vol.113, No.3, pp.590-596.

[2] 1996, Taslim, M.E., Li, T. and Kercher, D.M.,

"Experimental Heat Transfer and Friction in Channels Roughened with Angled, V shaped, and Discrete Ribs on Two Opposite Walls," Journal of Turbomachinery, Vol.119, pp.381-389.

[3] 1993, Kukreja, R.T., Lau, S.C. and Mcmillin, R.D., "Local

Heat/Mass Transfer Distribution in a Square Channel with Full and V shaped Ribs," International Journal of Heat and Mass Transfer, Vol.36, No.8, pp.2013-2020.

[4] 1997, Taslim, M.E. and Wadsworth, C.M., "An Experimental Investigation of the Rib Surface Avraged Heat Transfer Coefficient in a Rib Roughened Square Passage," Journal of Turbomachinery, Vol.119, pp.381-389.

[5] 2001, Cho, H.H., Lee, S.Y. and Wu, S.J., "The Combined Effects of Rib Arrangements and Discrete Ribs on Local Heat/Mass Transfer in a Square Duct," IGTI Turbo Expo Paper, No 2001-GT-0175, Louisiana, USA.

[6] 2002, Jia, R., Saidi, A. and Sunden, B., "Heat Transfer Enhancement in Square Ducts with V shaped Ribs of Various Angles," Proceedings of ASME TURBO EXPO 2002, Amsterdam, June 3~6, GT2002-30209.

[7] 2003, Su, G., Chen, H.C. and Han, J.C., "Computation of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4) with V shaped Ribs by A Reynolds Stress Turbulence Model," Proceedings of ASME TURBO EXPO 2003, Atlanta, June 16~19, GT-2003-38348.

[8] 2007, Kim, K.Y. and Lee, Y.M., "Design Optimization of Internal Cooling Passage with V-shaped Ribs," Numerical Heat Transfer, Part A, Vol.51, pp.1103-1118.

[9] 1996, Lopez, J.R., Anand, N.K. and Fletcher, L.S., "Heat Transfer in a Three-Dimensional Channel with Baffles,"

Numerical Heat Transfer, Part A, Vol.30, pp.189-205.

[10] 2006, Horiuchi, Y., Kizuka, N. and Marushima, S.,

"Improvement of Heat Transfer Performance of Turbulence Promoter Ribs," Proceedings of GT2006, ASME Turbo Expo 2006: Power for Land, Sea and Air, GT2006-91168.

[11] 1980, Gee, D.L. and Webb, R.L., "Forced Convection Heat Transfer in Helically Rib-Roughened Tubes," International Journal of Heat and Mass Transfer, Vol.23, pp.1645-1656.

[12] 2005, Fluent 6.2, User's Manual, Fluent Inc..

[13] 2001, Menter, F. and Esch, T., "Elements of Industrial Heat Transfer Predictions," Proceedings of 16th Bazilian Congress of Mechanical Engineering, Uberlandia, Brazil.

[14] 1997, Bardina, J.E., Huang, P.G. and Coakley, T.,

"Turbulence Modeling Validation," AIAA Paper 97-2121.

수치

Fig. 1 Schematic of the cooling duct with staggered V-shaped   rib and the top view with location of specified  sections
Fig. 4 B Section(Fig. 1  ) ,  .  (snaking flow) .  ,  .  . =2.8 ,  Fig. 4(a) B-1 Section,
Table 1 Summary of heat transfer performance comparison  with respect to  ratios for V-shape ribs

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