Abstract

The sweeping jet can be a promising candidate in film cooling applications since it has a large lateral jet spreading which can be considered an advantage when compared to the regular steady jet film cooling. Fluidic oscillators can generate a sweeping jet without the need for any moving parts. In addition, they can be more conveniently manufactured by additive manufacturing techniques. This two-part paper presents a numerical study to investigate the application of using air/mist sweeping jets in film cooling for protecting turbine airfoils. Part I focuses on validating the computational mode by comparing the thermal-flow and heat transfer behavior between steady and sweeping air-only jets to ensure they are consistent with published information. Part II focuses on the mist behavior and its effect on heat transfer enhancement in the sweeping jet film cooling by adding micro-liquid droplets. An unsteady Reynolds-averaged Navier–Stokes (URANS) simulation accompanied by the k–ω shear stress transport (SST) turbulence model was used in this study. A comparison is made between steady and sweeping jets at two blowing ratios (BR = 1 and 2). The results show that the steady jet provided better film cooling performance along the centerline compared to that of the sweeping jet for both blowing ratios. However, the sweeping jet provided better and more uniform film cooling performance in the spanwise direction. Both jets experienced a significant jet-liftoff when the blowing ratio was 2. The entrainment was significant in the sweeping jet case for both blowing ratios. The sweeping jet caused an increase of 9.5% in total pressure losses compared to the steady jet. It was found that for the sweeping jet, a pair of counter-rotating vortices is inward-rushing toward the wall in the center rather than outward-rushing as in a typical steady jet film cooling flow field. A detailed analysis is presented to understand the instantaneous vortex dynamics of the sweeping jet that leads to the inward rotating counter-rotating vortex pair (CRVP) (i.e., reversed CRVP). The result shows that the pair of counter-rotating vortices is just a time-averaged image of a single vortex sweeping back and forth in the domain; it does not actually exist in real time.

References

1.
Deadwyler
,
R.
,
1981
,
A Review of Models of the Fluidic Generator, U.S. Army Electronics Research and Development Command
,
Harry Diamond Laboratories
,
Adelphi, MD
.
2.
Viets
,
H.
,
1975
, “
Flip-Flop Jet Nozzle
,”
AIAA J.
,
13
(
10
), pp.
1375
1379
.
3.
Srinivas
,
T.
,
Vasudevan
,
B.
, and
Prabhu
,
A.
,
1988
, “Performance of Fluidically Controlled Oscillating Jet,”
Turbulence Management and Relaminarisation
,
Springer
,
Berlin
, pp.
485
494
.
4.
Gregory
,
J. W.
,
Sullivan
,
J. P.
,
Raman
,
G.
, and
Raghu
,
S.
,
2007
, “
Characterization of the Microfluidic Oscillator
,”
AIAA J.
,
45
(
3
), pp.
568
576
.
5.
Woszidlo
,
R.
,
Ostermann
,
F.
, and
Schmidt
,
H.
,
2019
, “
Fundamental Properties of Fluidic Oscillators for Flow Control Applications
,”
AIAA J.
,
57
(
3
), pp.
978
992
.
6.
Gregory
,
J. W.
, and
Tomac
,
M. N.
,
2013
, “
A Review of Fluidic Oscillator Development and Application for Flow Control
,”
43rd AIAA Fluid Dynamics Conference
, AIAA Paper No. 2013-2474.
7.
Shakouchi
,
T.
,
1989
, “
A New Fluidic Oscillator, Flowmeter, Without Control Port and Feedback Loop
,”
J. Dyn. Syst. Meas. Control
,
111
(
3
), pp.
535
539
.
8.
Ostermann
,
F.
,
Woszidlo
,
R.
,
Nayeri
,
C. N.
, and
Paschereit
,
C. O.
,
2016
, “
The Time-Resolved Flow Field of a Jet Emitted by a Fluidic Oscillator Into a Crossflow
,”
54th AIAA Aerospace Sciences Meeting
,
San Diego, CA
,
Jan. 4–8
,
AIAA 2016-0345
.
9.
Hossain
,
M. A.
,
Prenter
,
R.
,
Lundgreen
,
R. K.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
,
2018
, “
Experimental and Numerical Investigation of Sweeping Jet Film Cooling
,”
ASME J. Turbomach.
,
140
(
3
), p.
031009
.
10.
Ostermann
,
F.
,
Woszidlo
,
R.
,
Nayeri
,
C. N.
, and
Paschereit
,
C. O.
,
2018
, “
Properties of a Sweeping Jet Emitted From a Fluidic Oscillator
,”
J. Fluid Mech.
,
857
, pp.
216
238
.
11.
Aram
,
S.
,
Lee
,
Y.
,
Shan
,
H.
, and
Vargas
,
A.
,
2018
, “
Computational Fluid Dynamic Analysis of Fluidic Actuator for Active Flow Control Applications
,”
AIAA J.
,
56
(
1
), pp.
111
120
.
12.
Aram
,
S.
,
2020
, “
Numerical Analysis of Sweeping Jets for Active Flow Control Application
,”
ASME J. Fluids Eng.
,
142
(
3
), p.
030901
.
13.
Hossain
,
M. A.
,
Prenter
,
R.
,
Lundgreen
,
R. K.
,
Agricola
,
L.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
, “
Investigation of Crossflow Interaction of an Oscillating Jet
,”
55th AIAA Aerospace Sciences Meeting
,
Grapevine, TX
,
Jan. 9–13
,
AIAA 2017-1690
.
14.
Hossain
,
M. A.
,
Prenter
,
R.
,
Agricola
,
L.
,
Lundgreen
,
R. K.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
,
2017
, “
Effects of Roughness on the Performance of Fluidic Oscillators
,”
55th AIAA Aerospace Sciences Meeting
,
Grapevine, TX
,
Jan. 9–13
,
AIAA 2017-0770
.
15.
Hossain
,
M. A.
,
Agricola
,
L.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
,
2018
, “
Effects of Exit Fan Angle on the Heat Transfer Performance of Sweeping Jet Impingement
,”
International Energy Conversion Engineering Conference
,
Cincinnati, OH
,
July 9–11
,
AIAA 2018-4886
.
16.
Hossain
,
M. A.
,
Agricola
,
L.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
,
2018
, “
Effects of Curvature on the Performance of Sweeping Jet Impingement Heat Transfer
,”
AIAA Aerospace Sciences Meeting
,
Kissimmee, FL
,
Jan. 8–12
,
AIAA 2018-0243
.
17.
Thurman
,
D. R.
,
Culley
,
D. E.
,
Poinsatte
,
P.
,
Raghu
,
S.
,
Ameri
,
A.
, and
Shyam
,
V.
,
2016
, “
Investigation of Spiral and Sweeping Holes
,”
ASME J. Turbomach.
,
138
(
9
), p.
091007
.
18.
Shyam
,
V.
,
Thurman
,
D. R.
,
Poinsatte
,
P. E.
,
Ameri
,
A.
, and
Culley
,
D. E.
,
2018
, “
Toward Cooling Uniformity: Investigation of Spiral, Sweeping Holes, and Unconventional Cooling Paradigms
,” NASA/TM-2018-219763, E-19475, GRC-E-DAA-TN52180.
19.
Hossain
,
M. A.
,
Agricola
,
L.
,
Ameri
,
A.
,
Gregory
,
J. W.
, and
Bons
,
J. P.
,
2019
, “
Sweeping Jet Film Cooling on a Turbine Vane
,”
ASME J. Turbomach.
,
141
(
3
), p.
031007
.
20.
Abdelmaksoud
,
R.
, and
Wang
,
T.
,
2022
, “
Recent Advances in Heat Transfer Applications Using Sweeping Jet Fluidic Oscillators
,”
Int. J. Energy Clean Environ.
,
24
(
2
), pp.
21
87
.
21.
Menter
,
F. R.
,
1994
, “
Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications
,”
AIAA J.
,
32
(
8
), pp.
1598
1605
.
22.
Dhungel
,
A.
,
Lu
,
Y.
,
Phillips
,
W.
,
Ekkad
,
S. V.
, and
Heidmann
,
J.
,
2009
, “
Film Cooling From a Row of Holes Supplemented With Antivortex Holes
,”
ASME J. Turbomach.
,
131
(
2
), p.
021007
.
23.
He
,
Y. L.
, and
Zhang
,
Y.
,
2012
, “Chapter Two–Advances and Outlooks of Heat Transfer Enhancement by Longitudinal Vortex Generators,”
Advances in Heat Transfer
,
E. M.
Sparrow
,
Y. I.
Cho
,
J. P.
Abraham
, and
J. M.
Gorman
, eds.,
Elsevier
,
New York
, pp.
119
185
.
You do not currently have access to this content.