High solidity pin and pedestal arrays are beneficial in reducing temperature gradients and distributing stress across double wall cooling channels such as trailing edge regions. In this study two high solidity (45%) cooling channel geometries were selected and tested in both constant channel height and converging channel configurations. One geometry consisted of a high solidity round pin fin array and the other geometry consisted of a rounded diamond pedestal array designed to minimize pressure drop. Heat transfer rates for both geometries were determined on a row by row basis for both the constant channel and converging channel configurations. Heat transfer and pressure drop measurements were acquired in a bench scale test rig. Reynolds numbers ranged from approximately 3000 to 60,000 for the constant channel arrays and 3500 to 100,000 for the converging arrays based on the characteristic dimension of the pin or pedestal and the local maximum average velocity across a row. The high solidity pin fin array had an axial spacing (X/D) of 1.043 and a cross channel spacing (Z/D) of 1.674. The high solidity diamond pedestal array had an axial spacing of 1.00 and a cross channel spacing of 1.93. The constant section pin fin array had a channel height to diameter of 0.95 while the constant section diamond pedestal array had a height to characteristic dimension of 0.96. The converging pin fin array had an inlet to exit convergence ratio of 2.87 over five heated rows while the converging pedestal array had an inlet to exit convergence ratio of 3.53 over seven heated rows. The constant channel height internal cooling schemes have shown that the high solidity pin fin and the rounded diamond pedestal arrays produce comparable heat transfer and array pressure drop. Both the converging channel arrays show a noticeable (5–7%) reduction in heat transfer compared with the constant height channels. Array pressure drop for the two converging geometries was found to be quite consistent.

1.
Jaswal
,
I.
,
Erickson
,
E.
, and
Ames
,
F. E.
, 2009, “
Aerodynamics of a Covered Trailing Edge Vane—Effects of Blowing Rate, Reynolds Number, and External Turbulence
,” ASME Paper No. GT2009-59836.
2.
Metzger
,
D. E.
,
Shepard
,
W. B.
, and
Haley
,
S. W.
, 1986, “
Row Resolved Heat Transfer Variations in Pin Fin Arrays Including Effects of Non-Uniform Arrays and Flow Convergence
,” ASME Paper No. 86-GT-132.
3.
Metzger
,
D. E.
, and
Haley
,
S. W.
, 1982, “
Heat Transfer Experiments and Flow Visualization for Arrays of Short Pin Fins
,” ASME Paper No. 82-GT-138.
4.
Van Fossen
,
G. J.
, 1982, “
Heat-Transfer Coefficients for Staggered Arrays of Short Pin Fins
,”
ASME J. Eng. Power
0022-0825,
104
, pp.
268
274
.
5.
Chyu
,
M. K.
,
Hsing
,
Y. C.
,
Shih
,
T. I.-P.
, and
Natarajan
,
V.
, 1999, “
Heat Transfer Contributions of Pins and Endwall in Pin-Fin Arrays: Effects of Thermal Boundary Conditions Modeling
,”
ASME J. Turbomach.
0889-504X,
121
, pp.
257
263
.
6.
Ames
,
F. E.
,
Solberg
,
C. S.
,
Goman
,
M. D.
,
Curtis
,
D. J.
, and
Steinbrecker
,
B. T.
, 2001, “
Experimental Measurements and Computations of Heat Transfer and Friction Factor in a Staggered Pin Fin Array
,” ASME Paper No. DETC2001/CIE-21761.
7.
Chyu
,
M. K.
,
Yen
,
C. H.
, and
Siw
,
S.
, 2007, “
Comparison of Heat Transfer from Staggered Pin Fin Arrays with Circular, Cubic and Diamond Shaped Pins
,” ASME Paper GT2007-28306.
8.
Ames
,
F. E.
,
Dvorak
,
L. A.
, and
Morrow
,
M. J.
, 2005, “
Turbulent Augementation of Internal Convection of Pins in Staggered Pin Fin Arrays
,”
ASME J. Turbomach.
0889-504X,
127
, pp.
183
190
.
9.
Ames
,
F. E.
,
Nordquist
,
C. A.
, and
Klennert
,
L. A.
, 2007, “
Endwall Heat Transfer Measurements in a Staggered Pin Fin Array With an Adiabatic Pin
,” ASME Paper No. GT2007-27432.
10.
Hwang
,
J. -J.
, and
Liu
,
C. -C.
, 2002, “
Measurement of Endwall Heat Transfer and Pressure Drop in a Pin-Fin Wedge Duct
,”
Int. J. Heat Mass Transfer
0017-9310,
45
, pp.
877
889
.
11.
Ames
,
F. E.
,
Fiala
,
N. J.
, and
Johnson
,
J. D.
, 2007, “
Gill Slot Trailing Edge Heat Transfer—Effects of Blowing Rate, Reynolds Number, and External Turbulence on Heat Transfer and Film Cooling Effectiveness
,” ASME Paper No. GT2007-27397.
12.
Armstrong
,
J.
, and
Winstanley
,
D.
, 1988, “
A Review of Staggered Array Pin Fin Heat Transfer for Turbine Cooling Applications
,”
ASME J. Turbomach.
0889-504X,
110
, pp.
94
103
.
13.
]
Metzger
,
D. E.
,
Fan
,
C. S.
, and
Shepard
,
W. B.
, 1982, “
Pressure Loss and Heat Transfer Through Multiple Rows of Short Pins
,”
Heat Transfer
, Vol.
3
,
Hemisphere
,
Washington, DC
, pp.
137
142
.
14.
Jacob
,
M.
, 1938, “
Heat Transfer and Flow Resistance in Cross Flow of Gases Over Tube Banks
,”
Trans. ASME
0097-6822,
59
, pp.
384
386
.
15.
Ames
,
F. E.
,
Dvorak
,
L. A.
, 2006, “
The Influence of Reynolds Number and Row Position on Surface Pressure Distributions in Staggered Pin Fin Arrays
,” ASME Paper No. GT2006-90170.
16.
Grimison
,
E. D.
, 1937, “
Correlation and Utilization of New Data on Flow Resistance and Heat Transfer for Cross Flow of Gases Over Tube Banks
,”
Trans. ASME
0097-6822,
59
, pp.
583
594
.
17.
Miller
,
R. W.
, 1996,
Flow Measurement Engineering Handbook
, 3rd ed.,
McGraw-Hill
,
New York
.
18.
Moffat
,
R. J.
, 1988, “
Describing Uncertainties in Experimental Results
,”
Exp. Therm. Fluid Sci.
0894-1777,
1
, pp.
3
17
.
19.
Jaswal
,
I.
, 2008, “
Aerodynamic Losses and Heat Transfer for a Covered Trailing Edge Turbine Vane With a High Solidity Low Pressure Drop Pedestal Pin Fin Array and Variable Coolant Ejection
,” MA thesis, University of North Dakota, Grand Forks, ND.
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