Abstract

Heat transfer and pressure drop measurements are reported for a rotating 4:1 aspect ratio (AR) smooth two-pass coolant passage for Reynolds number in the range of 10,000–150,000, rotation number in the range of 0–0.6, and density ratios in the range of 0.1–0.2. The measurements are performed for both 90deg and 45deg orientations of the coolant passage relative to the rotational axis. A large-scale rotating heat transfer rig is utilized, with the test section consisting of segmented foil-heated elements and thermocouples. Results for the 4:1 AR indicate that beyond specific Ro values (different values for the inlet and outlet passages), the expected trends of heat transfer enhancement on the destabilized surface and degradation on the stabilized surface are arrested or reversed. Unlike the 1:1 AR, the inlet-leading surface for the 4:1 AR shows enhancement with Ro at low Re (less than 20,000) and shows the expected degradation only at high Re. Increasing the density ratio enhances the heat transfer on all walls. Orientation of the coolant passage relative to the rotational axis has an important effect, with the 45deg orientation reducing the heat transfer on the destabilized surface and enhancing it on the stabilized surface.

References

1.
Mori
,
Y.
,
Fukada
,
T.
, and
Nakayama
,
W.
, 1971, “
Convective Heat Transfer in a Rotating Circular Pipe (Second Report)
,”
Int. J. Heat Mass Transfer
0017-9310,
14
, pp.
1807
1824
.
2.
Metzger
,
D. E.
, and
Stan
,
R. L.
, 1977, “
Entry Region Heat Transfer in Rotating Radial Tubes
,”
J. Energy
0146-0412,
1
(
5
), pp.
297
300
.
3.
Morris
,
W. D.
, and
Ayhan
,
T.
, 1979, “
Observations on the Influence of Rotation On Heat Transfer in the Cooling Channels of Gas Turbine Rotor Blades
,”
Proc. Inst. Mech. Eng.
0020-3483,
193
, pp.
303
311
.
4.
Wagner
,
J. H.
,
Johnson
,
B. V.
, and
Hajek
,
T. J.
, 1991, “
Heat Transfer in Rotating Passages With Smooth Walls and Radial Outward Flow
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
42
51
.
5.
Wagner
,
J. H.
,
Johnson
,
B. V.
, and
Kopper
,
F. C.
, 1991, “
Heat Transfer in Rotating Serpentine Passages With Smooth Walls
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
321
330
.
6.
Mochizuki
,
S.
,
Takamura
,
J.
,
Yamawaki
,
S.
, and
Yang
,
W.-J.
, 1994, “
Heat Transfer in Serpentine Flow Passages With Rotation
,”
ASME J. Turbomach.
0889-504X,
116
, pp.
133
140
.
7.
Guidez
,
J.
, 1989, “
Study of the Convective Heat Transfer in a Rotating Coolant Channel
,”
ASME J. Turbomach.
0889-504X,
111
, pp.
43
51
.
8.
Morris
,
W. D.
, and
Ghavami-Nasr
,
G.
, 1991, “
Heat Transfer Measurements in Rectangular Channel With Orthogonal Mode Rotation
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
339
345
.
9.
Iacovides
,
H.
, and
Launder
,
B. E.
, 1991, “
Parametric and Numerical Study of Fully Developed Flow and Heat Transfer in Rotating Rectangular Ducks
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
331
338
.
10.
Soong
,
C. Y.
,
Lin
,
S. T.
, and
Hwang
,
G. J.
, 1991, “
An Experimental Study of Convective Heat Transfer in Radially Rotating Rectangular Ducts
,”
ASME J. Heat Transfer
0022-1481,
113
, pp.
604
611
.
11.
Griffith
,
T. S.
,
Al-Hadhrami
,
L.
, and
Han
,
J. C.
, 2002, “
Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Angled Ribs
,”
ASME J. Heat Transfer
0022-1481,
124
, pp.
1
9
.
12.
Kays
,
W. M.
, and
Crawford
,
M. E.
, 1993,
Convective Heat and Mass Transfer
, 3rd ed.,
McGraw-Hill
,
New York
.
13.
Kline
,
S. J.
, and
McClintock
,
F. A.
, 1953, “
Describing Uncertainties in Single-Sample Experiments
,”
Mech. Eng. (Am. Soc. Mech. Eng.)
0025-6501,
75
(
1
), pp.
3
8
.
14.
Han
,
J. C.
,
Park
,
J. S.
, and
Ibrahim
,
M. Y.
, 1986, “
Measurement of Heat Transfer and Pressure Drop in Rectangular Channels With Turbulence Promoters
,” NASA Contractor Report No. CR 4015.
15.
Saha
,
A.
, and
Acharya
,
S.
, 2004, “
Unsteady RANS Simulations of Turbulent Flow and Heat Transfer in Ribbed Coolant Passages of Different Aspect Ratios
,”
Int. J. Heat Mass Transfer
0017-9310,
48
(
23–24
), pp.
4704
4725
.
16.
Willett
,
F. T.
, and
Bergles
,
A. E.
, 2001, “
Heat Transfer in Rotating Narrow Rectangular Ducts With Heated Sides Oriented at 60deg to the R-Z Plan
,”
ASME J. Turbomach.
0889-504X,
123
, pp.
288
295
.
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