Motivated by the need to further improve film cooling in terms of both cooling effectiveness and coolant coverage area, the mist/air film cooling scheme is investigated through experiments using fan-shaped holes over an extended downstream length in this study. Both an existing wind tunnel and test facility, used in previous work, have been retrofitted. The first modification was extending the length of the flat plate test section to cover longer distances downstream of the injection holes, up to X/D = 100, in order to investigate whether mist cooling can be harnessed farther downstream where single-phase film cooling is not effective. X represents the axial distance downstream of the cooling hole of diameter D. The second modification was to incorporate fan-shaped (diffusion) holes which are proven to have a higher film cooling efficiency, than cylindrical holes. The objective is to investigate whether mist can further enhance the film cooling performance of the already highly effective fan-shaped holes. A phase Doppler particle analyzer (PDPA) system is employed to measure the droplet size, velocity, and turbulence information. An infrared camera and thermocouples are both used for temperature measurements. Part I is focused on the heat transfer result on the wall. The results show that, at low blowing ratios when the film is attached to the surface, the enhancement of the mist film cooling effectiveness, compared to the air-only case, on the centerline of the hole ranges from 40% in the near hole region to over 170% at X/D = 100. Due to the diffusive nature of the fan-shaped hole, the laterally averaged enhancement is on par with that on the centerline. The significant enhancement over the extended downstream distance from X/D = 40–100 is attributed to the evaporation time needed to evaporate all of the droplets. Each droplet acts as a cooling sink and flies over a distance before it completely vaporizes. This “distributed cooling” characteristic allows the water droplets to extend the cooling effects farther downstream from the injection location. At higher blowing ratios, when the cooling film is lifted off from the surface, the cooling enhancement drops below 40%. Although the enhancement in the near hole region X/D < 40 is about 20% lower than that achieved by using the cylindrical holes, the magnitudes of the mist adiabatic film cooling effectiveness using fan-shaped holes are still much higher than those of the cylindrical holes. Part II of this study is focused on analyzing the two-phase droplet multiphase flow behavior to explain the fundamental physics involved in the mist film cooling.

References

1.
Goldstein
,
R. J.
,
1971
,
Film Cooling: Advances in Heat Transfer
, Vol.
7
,
Academic Press
,
New York
, pp.
321
379
.
2.
Mayhew
,
J. E.
,
Baughn
,
J. W.
, and
Byerley
,
A. R.
,
2003
, “
The Effect of Freestream Turbulence on Film Cooling Effectiveness
,”
Int. J. Heat Fluid Flow
,
24
(
5
), pp.
669
679
.
3.
Walters
,
D. K.
, and
Leylek
,
J. H.
,
1997
, “
A Detailed Analysis of Film-Cooling Physics-Part 1: Streamwise Injection With Cylindrical Holes
,”
ASME
Paper No. 97-GT-269.
4.
Zhang
,
L. J.
, and
Pudupaty
,
R.
,
2000
, “
The Effects of Injection Angle and Hole Exit Shape on Turbine Nozzle Pressure Side Film Cooling
,”
ASME
Paper No. 2000-GT-247.
6.
Medic
,
G.
, and
Durbin
,
P. A.
,
2002
, “
Toward Improved Film Cooling Prediction
,”
ASME J. Turbomach.
,
124
(
2
), pp.
193
199
.
7.
Dunn
,
M. G.
,
1986
, “
Heat Flux Measurement for a Rotor of a Full Stage Turbine—Part I: Time Averaged Results
,”
ASME J. Turbomach.
,
108
(
1
), pp.
90
97
.
8.
Dunn
,
M. G.
,
George
,
W. K.
,
Rae
,
W. J.
,
Woodward
,
S. H.
,
Moller
,
J. C.
, and
Seymour
,
J. P.
,
1986
, “
Heat Flux Measurement for a Rotor of a Full Stage Turbine, Part II: Description of Analysis Technique and Typical Time-Resolved Measurements
,”
ASME J. Turbomach.
,
108
(
1
), pp.
98
107
.
9.
Takagi
,
T.
, and
Ogasawara
,
M.
,
1974
, “
Some Characteristics of Heat and Mass Transfer in Binary Mist Flow
,”
Fifth International Heat Transfer Conference
, Tokyo, Japan, Sept. 3–4, pp.
350
354
.
10.
Mori
,
Y.
,
Hijikata
,
K.
, and
Yasunaga
,
T.
,
1982
, “
Mist Cooling of Very Hot Tubules With Reference to Through-Hole Cooling of Gas Turbine Blades
,”
Int. J. Heat Mass Transfer
,
25
(
9
), pp.
1271
1278
.
11.
Janssen
,
J. M.
,
Florschuetz
,
L. W.
, and
Fizdon
,
J. P.
,
1986
, “
Heat Transfer to Two-Phase Air/Water Mixtures Flowing in Small Tubes With Inlet Disequilibrium
,” NASA Lewis Research Center, Cleveland, OH, Report No.
NASA CR 175076
.https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860013421.pdf
12.
Guo
,
T.
,
Wang
,
T.
, and
Gaddis
,
J. L.
,
2000
, “
Mist/Steam Cooling in a Heated Horizontal Tube—Part I: Experimental System
,”
ASME J. Turbomach.
,
122
(
2
), pp.
360
365
.
13.
Guo
,
T.
,
Wang
,
T.
, and
Gaddis
,
J. L.
,
2000
, “
Mist/Steam Cooling in a Heated Horizontal Tube—Part II: Results and Modeling
,”
ASME J. Turbomach.
,
122
(
2
), pp.
366
374
.
14.
Guo
,
T.
,
Wang
,
T.
, and
Gaddis
,
J. L.
,
2000
, “
Mist/Steam Cooling in a 180-Degree Tube
,”
ASME J. Heat Transfer
,
122
(
4
), pp.
749
756
.
15.
Nazarov
,
A. D.
,
Serov
,
A. F.
,
Terekhov
,
V. I.
, and
Sharov
,
K. A.
,
2009
, “
Experimental Investigation of Evaporative Pulse-Spray Impingement Cooling
,”
J. Eng. Phys. Thermophys.
,
82
(
6
), pp.
1184
1190
.
16.
Pakhomov
,
M. A.
, and
Terekhov
,
V. I.
,
2010
, “
Enhancement of an Impingement Heat Transfer Between Turbulent Mist Jet and Flat Surface
,”
Int. J. Heat Mass Transfer
,
53
(15–16), pp.
3156
3165
.
17.
Wang
,
T.
,
Gaddis
,
J. L.
, and
Li
,
X.
,
2005
, “
Mist/Steam Heat Transfer of Multiple Rows of Impinging Jets
,”
Int. J. Heat Mass Transfer
,
48
(25–26), pp.
5179
5191
.
18.
Nirmalan
,
N. V.
,
Weaver
,
J. A.
, and
Hylton
,
L. D.
,
1996
, “
An Experimental Study of Turbine Vane Heat Transfer With Water-Air Cooling
,”
ASME
Paper No. 96-GT-381.
19.
Li
,
X.
, and
Wang
,
T.
,
2006
, “
Simulation of Film Cooling Enhancement With Mist Injection
,”
ASME J. Heat Transfer
,
128
(
6
), pp.
509
519
.
20.
Li
,
X.
, and
Wang
,
T.
,
2007
, “
Effects of Various Modeling on Mist Film Cooling
,”
ASME J. Heat Transfer
,
129
(
4
), pp.
472
482
.
21.
Wang
,
T.
, and
Li
,
X.
,
2008
, “
Mist Film Cooling Simulation at Gas Turbine Operating Conditions
,”
Int. J. Heat Mass Transfer
,
51
(21–22), pp.
5305
5317
.
22.
Li
,
X.
, and
Wang
,
T.
,
2008
, “
Two-Phase Flow Simulation of Mist Film Cooling on Turbine Blades With Conjugate Internal Cooling
,”
ASME J. Heat Transfer
,
130
(
10
), p.
102901
.
23.
Dhanasekaran
,
T. S.
, and
Wang
,
T.
,
2012
, “
Simulation of Mist Film Cooling on Rotating Gas Turbine Blades
,”
ASME J. Heat Transfer
,
134
(
1
), p.
011501
.
24.
Terekhov
,
V. I.
, and
Pakhomov
,
M. A.
,
2005
, “
The Thermal Efficiency of Near-Wall Gas-Droplets Screens—Part I: Numerical Modeling
,”
Int. J. Heat Mass Transfer
,
48
(
9
), pp.
1747
1759
.
25.
Kanani
,
H.
,
Shams
,
M.
, and
Ebrahimi
,
R.
,
2009
, “
Numerical Modeling of Film Cooling With and Without Mist Injection
,”
Int. J. Heat Mass Transfer
,
45
(
6
), pp.
727
741
.
26.
Jiang
,
Y.
,
Zheng
,
Q.
,
Dong
,
P.
,
Yue
,
G.
, and
Gao
,
J.
,
2014
, “
Numerical Simulation on Turbine Blade Leading-Edge High-Efficiency Film Cooling by the Application of Water Mist
,”
Numer. Heat Transfer, Part A
,
66
(
12
), pp.
1341
1364
.
27.
Ragab
,
R.
, and
Wang
,
T.
,
2012
, “
An Investigation of Applicability of Transporting Water Mist for Cooling Turbine Vanes
,”
ASME
Paper No. GT2012-70110.
28.
Wang
,
T.
, and
Ragab
,
R.
,
2013
, “
Investigation of Applicability of Transporting Water Mist for Cooling Turbine Blades
,”
ASME
Paper No. GT2014-25818.
29.
Ragab
,
R.
, and
Wang
,
T.
,
2013
, “
Investigation of Applicability of Using Water Mist for Cooling High- Pressure Turbine Components Via Rotor Cavity Feed Channels
,”
ASME
Paper No. HT2013-17150.
30.
Bunker
,
R. S.
,
2005
, “
A Review of Shaped Hole Turbine Film-Cooling Technology
,”
ASME J. Heat Transfer
,
127
(4), pp. 441–453.
31.
Colban
,
W.
,
Thole
,
K. A.
, and
Haendler
,
M.
,
2006
, “
A Comparison of Cylindrical and Fan-Shaped Film-Cooling Holes on a Vane Endwall at Low and High Free Stream Turbulence Levels
,”
ASME
Paper No. GT2006-90021.
32.
Wang
,
T.
, and
Zhao
,
L.
,
2013
, “
Development of an Experimental Test Facility for Investigating Mist/Air Film Cooling Application in Gas Turbine Airfoils
,”
ASME
Paper No. GT2013-94476.
33.
Zhao
,
L.
, and
Wang
,
T.
,
2014
, “
An Experimental Study of Mist/Air Film Cooling on a Flat Plate With Application to Gas Turbine Airfoils—Part I: Heat Transfer
,”
ASME J. Turbomach.
,
136
(
7
), p.
071006
.
34.
Zhao
,
L.
, and
Wang
,
T.
,
2014
, “
An Experimental Study of Mist/Air Film Cooling On a Flat Plate With Application to GasTurbine Airfoils—Part II: Two-Phase Flow Measurements and Droplet Dynamics
,”
ASME J. Turbomach.
,
136
(
7
), p.
071007
.
35.
Chaker
,
M. A.
,
2005
, “
Key Parameters for The Performance of Impaction-Pin Nozzles Used in Inlet Fogging of Gas Turbine Engines
,”
ASME
Paper No. GT2005-68346.
36.
Ragab
,
R.
, and
Wang
,
T.
,
2013
, “
Experimental Investigation of Mist Film Cooling and Feasibility Study of Mist Transport in Gas Turbines
,”
Ph.D. thesis
, University of New Orleans, New Orleans, LA.http://scholarworks.uno.edu/td/1762/
37.
Moffat
,
R. J.
,
1982
, “
Contributions to the Theory of Single-Sample Uncertainty Analysis
,”
SME J. Fluids Eng.
,
104
(
2
), pp.
250
260
.
38.
Wang
,
T.
, and
Simon
,
W.
,
1989
, “
Development of a Special-Purpose Test Surface Guided by Uncertainty Analysis
,”
AIAA J. Thermophys. Heat Transfer
,
3
(
1
), pp.
19
26
.
You do not currently have access to this content.