This paper reports on quantitative tests of passive techniques for rotor-tip noise control in low-speed axial flow fans, based on blade-tip modifications involving the addition of antivortex appendages as end-plates. The end-plate thickness chordwise distribution is determined to control the chordwise evolution of the leakage vortex rotation number. The results confirm that the new end-plate configurations provide a mechanism by which leakage vortex bursting can be avoided. As such, the modified rotors represent an effective means of passive control of vortex breakdown.

1.
Fukano
,
T.
, and
Takamatsu
,
Y.
, 1986, “
The Effects of Tip Clearance on the Noise of Low-Pressure Axial and Mixed Flow Fans
,”
J. Sound Vib.
0022-460X,
105
, pp.
291
308
.
2.
Furukawa
,
M.
,
Inoue
,
M.
,
Kuroumaru
,
M.
,
Saiki
,
K.
, and
Yamada
,
K.
, 1999, “
The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics
,”
ASME J. Turbomach.
0889-504X,
121
, pp.
469
480
.
3.
Storer
,
J. A.
, and
Cumpsty
,
N. A.
, 1991, “
Tip Leakage Flow in Axial Compressors
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
252
259
.
4.
Ganz
,
U. W.
,
Joppa
,
P. D.
, and
Scharpf
,
D. F.
, 1998,
Boeing 18-Inch Fan Rig Broadband Noise Test
,
NASA
Report No. CR-1998-208704.
5.
Takata
,
H.
, and
Tsukuda
,
Y.
, 1977, “
Stall Margin Improvement by Casing Treatment—Its Mechanism and Effectiveness
,”
ASME J. Eng. Power
0022-0825,
99
, pp.
121
133
.
6.
Smith
,
G. D. J.
, and
Cumpsty
,
N. A.
, 1984, “
Flow Phenomena in Compressor Casing Treatment
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
106
, pp.
532
541
.
7.
Thompson
,
D. W.
,
King
,
P. I.
, and
Rabe
,
D. C.
, 1998, “
Experimental and Computational Investigation on Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor
,”
ASME J. Turbomach.
0889-504X,
120
, pp.
477
486
.
8.
Jensen
,
C. E.
, 1986, “
Axial-Flow Fan
,” U.S. Patent No. 4,630,993.
9.
Quinlan
,
D. A.
, and
Bent
,
P. H.
, 1998, “
High Frequency Noise Generation in Small Axial Flow Fans
,”
J. Sound Vib.
0022-460X,
218
, pp.
177
204
.
10.
Longet
,
C. M. L.
, 2003, “
Axial Flow Fan With Noise Reducing Means
,” U.S. Patent No. 2003/0123987 A1.
11.
Mimura
,
M.
, 2003, “
Axial Flow Fan
,” U.S. Patent No. 6,648,598 B2.
12.
Uselton
,
R. B.
,
Cook
,
L. J.
, and
Wright
,
T.
, 2005, “
Fan With Reduced Noise Generation
,” U.S. Patent No. 2005/0147496 A1.
13.
Corsini
,
A.
,
Perugini
,
B.
,
Rispoli
,
F.
,
Kinghorn
,
I.
, and
Sheard
,
A. G.
, 2006, “
Investigation on Improved Blade Tip Concept
,” ASME Paper No. GT2006-90592.
14.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2007, “
Development of Improved Blade Tip Endplate Concepts for Low-Noise Operation in Industrial Fans
,”
Proc. Inst. Mech. Eng., Part A
0957-6509,
221
(
5
), pp.
669
681
.
15.
Corsini
,
A.
,
Perugini
,
B.
,
Rispoli
,
F.
,
Kinghorn
,
I.
, and
Sheard
,
A. G.
, 2007, “
Experimental and Numerical Investigations on Passive Devices for Tip-Clearance Induced Noise Reduction in Axial Flow Fans
,”
Proceedings of the Seventh European Conference on Turbomachinery
, Athens, Greece.
16.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2008, “
A Meridional Fan
,” Patent Application No. GB 0800582.9, pending.
17.
Spall
,
R. E.
,
Gatski
,
T. B.
, and
Grosch
,
C. E.
, 1987, “
A Criterion for Vortex Breakdown
,”
Phys. Fluids
0031-9171,
30
(
11
), pp.
3434
3440
.
18.
Escudier
,
M.
, 1987, “
Confined Vortices in Flow Machinery
,”
Annu. Rev. Fluid Mech.
0066-4189,
19
, pp.
27
52
.
19.
Herrada
,
M. A.
, and
Shtern
,
V.
, 2003, “
Vortex Breakdown Control by Adding Near-Axis Swirl and Temperature Gradients
,”
Phys. Rev. E
1063-651X,
68
, p.
041202
.
20.
Jones
,
M. C.
,
Hourigan
,
K.
, and
Thompson
,
M. C.
, 2001, “
The Generation and Suppression of Vortex Breakdown by Upstream Swirl Perturbations
,”
Proceedings of the 14th Australian Fluid Mechanics Conference
, Adelaide, Australia.
21.
Srigrarom
,
S.
, and
Kurosaka
,
M.
, 2000, “
Shaping of Delta-Wing Planform to Suppress Vortex Breakdown
,”
AIAA J.
0001-1452,
38
, pp.
183
186
.
22.
Inoue
,
M.
,
Kuroumaru
,
M.
, and
Furukawa
,
M.
, 1986, “
Behavior of Tip Leakage Flow Behind an Axial Compressor Rotor
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
108
, pp.
7
14
.
23.
Corsini
,
A.
, and
Rispoli
,
F.
, 2004, “
Using Sweep to Extend Stall-Free Operational Range in Sub-Sonic Axial Fan Rotors
,”
Proc. Inst. Mech. Eng., Part A
0957-6509,
218
, pp.
129
139
.
24.
Borello
,
D.
,
Corsini
,
A.
, and
Rispoli
,
F.
, 2003, “
A Finite Element Overlapping Scheme for Turbomachinery Flows on Parallel Platforms
,”
Comput. Fluids
0045-7930,
32
(
7
), pp.
1017
1047
.
25.
Craft
,
T. J.
,
Launder
,
B. E.
, and
Suga
,
K.
, 1996, “
Development and Application of a Cubic Eddy-Viscosity Model of Turbulence
,”
Int. J. Heat Fluid Flow
0142-727X,
17
, pp.
108
155
.
26.
Corsini
,
A.
,
Rispoli
,
F.
, and
Santoriello
,
A.
, 2005, “
A Variational Multi-Scale High-Order Finite Element Formulation for Turbomachinery Flow Computations
,”
Comput. Methods Appl. Mech. Eng.
0045-7825,
194
(
45–47
), pp.
4797
4823
.
27.
Lucca-Negro
,
O.
, and
O’Doherty
,
T.
, 2001, “
Vortex Breakdown: A Review
,”
Prog. Energy Combust. Sci.
0360-1285,
27
, pp.
431
481
.
28.
Leibovich
,
S.
, 1978, “
The Structure of Vortex Breakdown
,”
Annu. Rev. Fluid Mech.
0066-4189,
10
, pp.
221
246
.
29.
Escudier
,
M.
, and
Zehnder
,
N.
, 1982, “
Vortex Flow Regimes
,”
J. Fluid Mech.
0022-1120,
115
, pp.
105
121
.
30.
Inoue
,
M.
, and
Furukawa
,
M.
, 2002, “
Physics of Tip Clearance Flow in Turbomachinery
,” ASME Paper No. FEDSM2002-31184.
31.
Leibovich
,
S.
, 1982, “
Wave Propagation, Instability, and Breakdown of Vortices
,”
Vortex Motion
,
M.
Hornung
, ed.,
Braunschweig
,
Vieweg
, pp.
50
67
.
32.
Benjamin
,
T. B.
, 1962, “
Theory of the Vortex Breakdown Phenomenon
,”
J. Fluid Mech.
0022-1120,
14
, pp.
593
629
.
33.
Tsai
,
C. -Y.
, and
Widnall
,
S. E.
, 1980, “
Examination of Group-Velocity Criterion for Breakdown of Vortex Flow in a Divergent Duct
,”
Phys. Fluids
0031-9171,
23
, pp.
864
870
.
34.
Ito
,
T.
,
Suematsu
,
Y.
, and
Hayase
,
T.
, 1985, “
On the Vortex Breakdown Phenomena in a Swirling Pipe-Flow
,”
Nagoya University, Faculty of Engineering, Memoirs
,
37
(
2
), pp.
117
172
. 0027-7657
35.
Leibovich
,
S.
, 1984, “
Vortex Stability and Breakdown: Survey and Extension
,”
AIAA J.
0001-1452,
22
, pp.
1192
1206
.
36.
Uchida
,
S.
,
Nakamura
,
Y.
, and
Ohsawa
,
M.
, 1985, “
Experiments on the Axisymmetric Vortex Breakdown in a Swirling Air Flow
,”
Trans. Jpn. Soc. Aeronaut. Space Sci.
0549-3811,
27
(
78
), pp.
206
216
.
37.
Garg
,
A. K.
, and
Leibovich
,
S.
, 1979, “
Spectral Characteristics of Vortex Breakdown Flowfields
,”
Phys. Fluids
0031-9171,
22
(
11
), pp.
2053
2064
.
38.
Gbadebo
,
S. A.
,
Cumpsty
,
N. A.
, and
Hynes
,
T. P.
, 2006, “
Interaction of Tip Clearance Flow and Three-Dimensional Separations in Axial Compressors
,” ASME Paper No. GT2006-90071.
39.
Corsini
,
A.
, and
Sheard
,
A. G.
, 2007, “
Tip End-Plate Concept Based on Leakage Vortex Rotation Number Control
,”
Comput. Appl. Math.
0101-8205,
8
(
1
), pp.
21
37
.
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