While the measurement of drag and lift forces on a body in external flow is common practice, the same cannot be said for aerodynamic forces on bodies in internal flows. The inherent difficulty in making force measurements on a body in an internal channel flow is decoupling the body from the bounding walls. The methodology presented in this paper uses a technique to overcome this constraint to accurately measure two components of force on a single cylinder within a single row array, with an aspect ratio (height-to-diameter ratio) of 1. Experiments were conducted with air over a range of Reynolds numbers between 7500 and 35,000 and for three different spanwise pin spacings. Experimental results indicated an increase in cylinder drag with a reduction in spanwise pin spacing. The gas turbine and electronics industries use cylinders or pin fins in internal flow channels to increase heat transfer augmentation through high turbulence and increased surface area. The flow fields in these obstructed channels are difficult to predict, so these measurements can be used to directly compare with predicted drag and lift forces.

1.
Munson
,
B. R.
,
Young
,
D. F.
, and
Okiishi
,
T. H.
, 2002,
Fundamentals of Fluid Mechanics
, 4th ed.,
Wiley
,
New York
, pp.
578
592
.
2.
Ames
,
F. E.
,
Dvorak
,
L. A.
, and
Morrow
,
M. J.
, 2005, “
Turbulent Augmentation of Internal Convection Over Pins in Staggered Pin Fin Arrays
,”
ASME J. Turbomach.
0889-504X,
127
(
1
), pp.
183
190
.
3.
Ames
,
F. E.
, and
Dvorak
,
L. A.
, 2006, “
The Influence of Reynolds Number and Row Position on Surface Pressure Distributions in Staggered Pin Fin Arrays
,”
ASME Turbo Expo 2006, Power for Land, Sea and Air
, Barcelona, Spain, Vol.
3
, Paper No. GT2006-90170, pp.
149
159
.
4.
Schetz
,
J. A.
, 2004, “
Direct Measurement of Skin Friction in Complex Flows Using Movable Wall Elements
,”
24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
, Portland, OR, Paper No. AIAA-2004-2112, Vol.
1
.
5.
De Turris
,
D. J.
,
Schetz
,
J. A.
, and
Hellbaum
,
R. F.
, 1990, “
Direct Measurements of Skin Friction in a SCRAMjet Combustor
,”
AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference
, Orlando, FL, Vol.
14
, AIAA Paper No. 1990-2342.
6.
Kakac
,
S.
,
Shah
,
R. K.
, and
Aung
,
W.
, 1987,
Handbook of Single Phase Convective Heat Transfer
,
Wiley
,
New York
, pp.
61
63
, Chap. 4.
7.
Kistler Morse
, 1998, “
Displacement Sensor (DS-6) Inspection and Operation Instructions
,” Kistler Morse, Report No. 97-2007-01.
8.
ASTM International
, 2002, “
Standard Practices of Calibration of Force-Measuring Instruments for Verifying the Force Indication of Testing Machines
,” ASTM E74-02, West Conshohocken, PA.
9.
2001, “
Product Information: Dow Corning 200 Fluid
,” Dow Corning Corporation, Report No. 10-1280-01.
10.
Moffat
,
R. J.
, 1988, “
Describing the Uncertainties in Experimental Results
,”
Exp. Therm. Fluid Sci.
0894-1777,
1
(
1
), pp.
3
17
.
11.
Goldstein
,
S.
, 1938,
Modern Developments in Fluid Dynamics: An Account of Theory and Experiment Relating to Boundary Layers, Turbulent Motion, and Wakes
,
Clarendon
,
Oxford
, pp.
418
440
.
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