While pressure sensitive paint (PSP) technique has been widely used to measure adiabatic film cooling effectiveness distributions on the surfaces of interest based on a mass transfer analog to traditional thermal-based measurements, very little can be found in literature to provide a comprehensive analysis on the uncertainty levels of the measured film cooling effectiveness distributions derived from PSP measurements. In the present study, a detailed analysis is performed to evaluate the effects of various associated uncertainties in the PSP measurements on the measured film cooling effectiveness distributions over the surfaces of interest. The experimental study is conducted in a low-speed wind tunnel under an isothermal condition. While airflow is used to represent the “hot” mainstream flow, an oxygen-free gas, i.e., carbon dioxide (CO2) gas with a density ratio of DR = 1.5 for the present study, is supplied to simulate the “coolant” stream for the PSP measurements to map the adiabatic film cooling effectiveness distribution over a flat test plate with an array of five cylindrical coolant holes at a span-wise spacing of three diameters center-to-center. A comprehensive analysis was carried out with focus on the measurement uncertainty and process uncertainty for the PSP measurements to determine the film cooling effectiveness distributions over the surface of interest. The final analysis indicates that the total uncertainty in the adiabatic film cooling effectiveness measurements by using the PSP technique depends strongly on the local behavior of the mixing process between the mainstream and coolant flows. The measurement uncertainty is estimated as high as 5% at the near field behind the coolant holes. In the far field away from the coolant holes, the total measurement uncertainty is found to be more uniform throughout the measurement domain and generally lower than those in the near field at about 3%.

References

1.
Baldauf
,
S.
,
Schulz
,
A.
, and
Wittig
,
S.
,
2001
, “
High-Resolution Measurements of Local Heat Transfer Coefficients From Discrete Hole Film Cooling
,”
ASME J. Turbomach.
,
123
(
4
), pp.
749
757
.
2.
Baldauf
,
S.
,
Schulz
,
A.
, and
Wittig
,
S.
,
2001
, “
High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling
,”
ASME J. Turbomach.
,
123
(
4
), pp.
758
765
.
3.
Wright
,
L. M.
,
Gao
,
Z.
,
Varvel
,
T. A.
, and
Han
,
J.-C.
,
2005
, “
Assessment of Steady State PSP, TSP, and IR Measurement Techniques for Flat Plate Film Cooling
,”
ASME
Paper No. HT2005-72363.
4.
Han
,
J.-C.
,
Dutta
,
S.
, and
Ekkad
,
S.
,
2012
,
Gas Turbine Heat Transfer and Cooling Technology
, 2nd ed.,
CRC Press
,
Boca Raton, FL
.
5.
Silieti
,
M.
,
Kassab
,
A. J.
, and
Divo
,
E.
,
2009
, “
Film Cooling Effectiveness: Comparison of Adiabatic and Conjugate Heat Transfer CFD Models
,”
Int. J. Therm. Sci.
,
48
(
12
), pp.
2237
2248
.
6.
Knost
,
D. G.
, and
Thole
,
K. A.
,
2003
, “
Computational Predictions of Endwall Film-Cooling for a First Stage Vane
,”
ASME
Paper No. GT2003-38252.
7.
Saumweber
,
C.
,
Schulz
,
A.
, and
Wittig
,
S.
,
2002
, “
Free-Stream Turbulence Effects on Film Cooling With Shaped Holes
,”
ASME
Paper No. GT2002-30170.
8.
Chyu
,
M. K.
,
Hsing
,
Y. C.
, and
Bunker
,
R. S.
,
1998
, “
Measurements of Heat Transfer Characteristics of Gap Leakage Around a Misaligned Component Interface
,”
ASME
Paper No. 98-GT-132.
9.
Kunze
,
M.
,
Preibisch
,
S.
,
Vogeler
,
K.
,
Landis
,
K.
, and
Heselhaus
,
A.
,
2008
, “
A New Test Rig for Film Cooling Experiments on Turbine Endwalls
,”
ASME
Paper No. GT2008-51096.
10.
Pedersen
,
D. R.
,
Eckert
,
E. R. G.
, and
Goldstein
,
R. J.
,
1977
, “
Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy
,”
ASME J. Heat Transfer
,
99
(
4
), p.
620
.
11.
Zhang
,
L. J.
, and
Jaiswal
,
R. S.
,
2001
, “
Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint
,”
ASME J. Turbomach.
,
123
(
4
), p.
730
.
12.
Ahn
,
J.
,
Mhetras
,
S.
, and
Han
,
J.
,
2005
, “
Film-Cooling Effectiveness on a Gas Turbine Blade Tip Using Pressure-Sensitive Paint
,”
ASME J. Heat Transfer
,
127
(
5
), pp.
521
530
.
13.
Charbonnier
,
D.
,
Ott
,
P.
,
Jonsson
,
M.
,
Cottier
,
F.
, and
Koübke
,
T.
,
2009
, “
Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform
,”
ASME
Paper No. GT2009-60306.
14.
Yang
,
Z.
, and
Hu
,
H.
,
2011
, “
Study of Trailing-Edge Cooling Using Pressure Sensitive Paint Technique
,”
J. Propul. Power
,
27
(
3
), pp.
700
709
.
15.
Yang
,
Z.
, and
Hu
,
H.
,
2012
, “
An Experimental Investigation on the Trailing Edge Cooling of Turbine Blades
,”
Propul. Power Res.
,
1
(
1
), pp.
36
47
.
16.
Rallabandi
,
A. P.
,
Grizzle
,
J.
, and
Han
,
J.-C.
,
2011
, “
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP
,”
ASME J. Turbomach.
,
133
(
4
), p.
041024
.
17.
Zhang
,
L. J.
, and
Fox
,
M.
,
1999
, “
Flat Plate Film Cooling Measurement Using PSP and Gas Chromatograph Techniques
,”
5th ASME/JSME Thermal Engineering Joint Conference
, San Diego, CA, Mar. 14–19, American Society of Mechanical Engineers, New York.
18.
Johnson
,
B.
,
Tian
,
W.
,
Zhang
,
K.
, and
Hu
,
H.
,
2014
, “
An Experimental Study of Density Ratio Effects on the Film Cooling Injection From Discrete Holes by Using PIV and PSP Techniques
,”
Int. J. Heat Mass Transfer
,
76
, pp.
337
349
.
19.
Natsui
,
G.
,
Little
,
Z.
,
Kapat
,
J. S.
,
Dees
,
J. E.
, and
Laskowski
,
G.
,
2015
, “
A Detailed Uncertainty Analysis of Adiabatic Film Cooling Effectiveness Measurements Using Pressure Sensitive Paint
,”
ASME
Paper No. GT2015-42707.
20.
Liu
,
T.
, and
Sullivan
,
J. P.
,
2005
,
Pressure and Temperature Sensitive Paints
,
Springer-Verlag
,
Berlin, Germany
.
21.
Wright
,
L. M.
,
McClain
,
S. T.
, and
Clemenson
,
M. D.
,
2011
, “
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP
,”
ASME J. Turbomach.
,
133
(
4
), p.
041011
.
22.
Han
,
J.-C.
, and
Rallabandi
,
A.
,
2010
, “
Turbine Blade Film Cooling Using PSP Technique
,”
Front. Heat Mass Transfer
,
1
(
1
), p.
013001
.
23.
Liu
,
K.
,
Yang
,
S.-F.
, and
Han
,
J.-C.
,
2012
, “
Influence of Coolant Density on Turbine Blade Film-Cooling With Axial Shaped Holes
,”
ASME
Paper No. HT2012-58144.
24.
Coleman
,
H.
, and
Steele
,
W.
,
2009
,
Experimentation, Validation, and Uncertainty Analysis for Engineers
,
Wiley
,
New York
.
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