Abstract

This study investigates the causal relationship between flow aerodynamics and radiated noise in low-speed axial fans. Using blades with three distinctive tip configurations, including two that were developed with a view to reducing noise emissions, the pressure fluctuations of the exhaust flow in the near field are correlated with the noise measured in the far field in an anechoic chamber. By varying the far-field microphone’s azimuthal position, the study investigates the source signatures and directivity of noise sources distributed along the blade span. Several distinctive features in the noise directivity pattern are identified and correlated with the noise sources of aerodynamic origin dissected along the blade span. Utilizing the directional far-field autospectra of the three blade configurations in combination with the near-field/far-field cross-spectra, the emission characteristics of the aerodynamic sources are analyzed and their roles with respect to the overall acoustic signature of the fan are discussed. It is apparent that the ability to decompose the output of the aerodynamic noise sources in the near field is a useful tool in designing fans to achieve desirable low-noise targets. The results confirm that the tip-flow appendages influence the noise radiation pattern for the investigated family of fans. These phenomena are linked with the control of aerodynamic noise sources related to the tip-leakage vortex and the hub corner separation.

1.
Wright
,
S. E.
, 1976, “
The Acoustic Spectrum of Axial Flow Machines
,”
J. Sound Vib.
0022-460X,
45
(
2
), pp.
165
223
.
2.
Cumpsty
,
N. A.
, 1977, “
A Critical Review of Turbomachinery Noise
,”
ASME J. Fluids Eng.
0098-2202,
99
, pp.
278
293
.
3.
Jordan
,
P.
, and
Gervais
,
Y.
, 2007, “
Subsonic Jet Aeroacoustics: Associating Experiments, Modelling and Simulations
,”
Exp. Fluids
0723-4864,
44
, pp.
1
21
.
4.
Mankbadi
,
R.
, and
Liu
,
J. T. C.
, 1984, “
Sound Generated Aerodynamically Revisited: Large-Scale Structures in a Turbulent Jet as a Source of Sound
,”
Philos. Trans. R. Soc. London, Ser. A
0962-8428,
311
, pp.
183
217
.
5.
Tam
C. K. Z.
, and
Golebiowski
,
S. J. M.
, 1996, “
On the Two Components of Turbulent Mixing Noise From Supersonic Jets
,” AIAA Paper No. 96-1716.
6.
Laurendeau
,
E.
,
Jordan
,
P.
,
Delville
,
J.
, and
Bonnet
,
J.
, 2007, “
Nearfield-Farfield Correlations in Subsonic Jets: What Can They Tell Us?
,” AIAA Paper No. 2007-3614.
7.
Lighthill
,
M. J.
, 1952, “
On Sound Generated Aerodynamically. I. General Theory
,”
Proc. R. Soc. London, Ser. A
0950-1207,
211
, pp.
564
587
.
8.
Lighthill
,
M. J.
, 1954, “
On Sound Generated Aerodynamically. II. Turbulence as a Source of Sound
,”
Proc. R. Soc. London, Ser. A
0950-1207,
222
, pp.
1
32
.
9.
Shah
,
P. D.
,
Mobed
,
D.
,
Spakovszky
,
Z.
, and
Brooks
,
T. F.
, 2007, “
A Novel Turbomachinery Air-Brake Concept for Quiet Aircraft
,”
ASME
Paper No. GT2007-27635.
10.
Shah
,
P. D.
,
Mobed
,
D.
,
Spakovszky
,
Z.
, and
Brooks
,
T. F.
, 2007, “
Aero-Acoustics of Drag Generating Swirling Exhaust Flows
,”
13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference)
, Rome, Italy, AIAA Paper No. 2007-3714.
11.
Tester
,
B. J.
, and
De Mercato
,
L.
, 2006, “
Far-Field Directivity of Rotor-Alone Tones Radiated From Fan Intakes With Spliced Liners for Different Intake Shapes, With Flow
,
12th AIAA/CEAS Aeroacoustics Conference
, Cambridge, MA.
12.
Heidelberg
,
L. J.
,
Sutliff
,
D. L.
, and
Nallasamy
,
M.
, 1997, “
Azimuthal Directivity of Fan Tones Containing Multiple Modes
,”
NASA
Report No. TM-107464.
13.
Julliard
,
J.
,
Antoine
,
H.
,
Lozachmeur
,
C.
, and
Roure
,
A.
2001,
Active Control of the Directivity of Fan Tones Noise, French Minister of Defense-Defense Technical Information Report
, Compilation Part Notice ADP011116.
14.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
A. G.
, 2007, “
Development of Improved Blade Tip End-Plate Concepts for Low-Noise Operation in Industrial Fans
,”
Proc. Inst. Mech. Eng., Part A
0957-6509,
221
(
5
), pp.
669
681
.
15.
Corsini
,
A.
, and
Sheard
,
A. G.
, 2007, “
Tip End-Plate Concept Based on Leakage Vortex Rotation Number Control
,”
J. Comput. Appl. Math.
0377-0427,
8
(
1
), pp.
21
37
.
16.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2010, “
Shaping of Tip End-Plate to Control Leakage Vortex Swirl in Axial Flow Fans
,”
ASME J. Turbomach.
0889-504X,
132
(
3
), p.
031005
.
17.
Bianchi
,
S.
,
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2009, “
Experimental Aeroacoustic Studies on Improved Tip Geometries for Passive Noise Signature Control in Low-Speed Axial Fans
,”
ASME J. Vibr. Acoust.
0739-3717,
131
(
6
), p.
061007
.
18.
Bianchi
,
S.
,
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2009, “
Detection of Aerodynamic Noise Sources in Low-Speed Axial Fans With Tip End-Plates
,”
Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci.
0954-4062,
223
(
6
), pp.
1379
1392
.
19.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2009, “
A Meridional Fan
,” International Patent Application No. PCT/GB2009/000088.
20.
Uchida
,
S.
,
Nakamura
,
Y.
, and
Oshawa
,
M.
, 1985, “
Experiments on the Axi-Symmetric Vortex Breakdown in a Swirling Air Flow
,”
Trans. Jpn. Soc. Aeronaut. Space Sci.
0549-3811,
27
(
78
), pp.
206
216
.
21.
Garg
,
A. K.
, and
Leibovich
,
S.
, 1979, “
Spectral Characteristics of Vortex Breakdown Flowfields
,”
Phys. Fluids
1070-6631,
22
, pp.
2053
2064
.
22.
ISO (2000), BS 848-2.6:2000, (2000), ISO 10302:1996, Fans for General Purposes. Methods of Noise Testing.
23.
ISO IEC60651, IEC/EN-61672-1, Calibration Rules for Hardware in Noise Measurements.
24.
Leggat
,
L. J.
, and
Siddon
,
T. E.
, 1978, “
Experimental Study of Aeroacoustic Mechanism of Rotor-Vortex Interactions
,”
J. Acoust. Soc. Am.
0001-4966,
64
, pp.
1070
1077
.
25.
Brüel & Kjaer
, 2006, 4954 1/2 inch Prepolarized Free-Field Microphone Manual.
26.
Miles
J. H.
, 2006, “
Procedure for Separating Noise Sources in Measurements of Turbofan Engine Core Noise
,”
NASA
Report No. TM-2006-214352.
27.
Bianchi
,
S.
,
Sheard
,
A. G.
,
Kinghorn
,
I. R.
,
Corsini
,
A.
, and
Rispoli
,
F.
, 2009, “
Experimental Development of a Measurement Technique to Resolve the Radial Distribution of Fan Aero-Acoustic Emissions
,”
Noise Control Eng. J.
0736-2501,
57
(
4
), pp.
360
369
.
28.
Blake
,
W. K.
, 1986,
Mechanics of Flow-Induced Sound and Vibration
,
Academic
,
Orlando, FL
, Vol.
II
.
29.
Widnall
,
S. E.
, 1969, “
A Correlation of Vortex Noise Data From Helicopter Main Rotors
,”
J. Aircr.
0021-8669,
6
, pp.
279
281
.
30.
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
.
31.
Longhouse
,
R. E.
, 1978, “
Control Tip-Vortex Noise of Axial Flow Fans by Rotating Shrouds
,”
J. Sound Vib.
0022-460X,
58
, pp.
201
214
.
32.
Nash
,
E. C.
,
Lowson
,
M. V.
, and
McAlpine
,
A.
, 1999, “
Boundary-Layer Instability Noise on Aerofoils
,”
J. Fluid Mech.
0022-1120,
382
, pp.
27
61
.
33.
Corsini
,
A.
,
Rispoli
,
F.
, and
Sheard
,
A. G.
, 2009, “
Aerodynamic Performance of Blade Tip End-Plates Designed for Low-Noise Operation in Axial Flow Fans
,”
ASME J. Fluids Eng.
0098-2202,
131
(
8
), p.
081101
.
34.
Möhring
,
W.
,
Muller
,
E.
, and
Obermeier
,
F.
, 1983, “
Problems in Flow Acoustics
,”
Rev. Mod. Phys.
0034-6861,
55
(
3
), pp.
707
724
.
You do not currently have access to this content.