This paper is conceived as an extension in the analysis of the periodic stator-rotor interaction in a low-speed axial fan with inlet guide vanes. Here, the present work focuses on the deterministic fluctuations that occur in the axial gap between the blade rows. In particular, we present experimental data on the phase averaged velocity in the stator frame of reference. Detailed measurements of the flow field were obtained using hot-wire anemometry in a traverse sector that covered the whole span of the stage for a complete stator pitch. The blade-to-blade velocity gradient in the rotor passage is observed as an unsteady flow in the stator frame of reference due to the relative motion of the blades. As a consequence, this periodic fluctuation is superimposed on the steady vane-to-vane velocity distribution, resulting in a nonuniform unsteadiness with additional phase-dependent wake-blockage interaction. This phase-dependent interaction is determined by the difference between the overall deterministic fluctuation and the rotating spatial blade-to-blade distribution, when the latter is accurately transformed to the stator reference frame. The results revealed that high unsteadiness in the tip region is mainly derived from the radial increase of the blade-to-blade nonuniformities in the rotor, whereas the wake-blockage interaction exhibits a spanwise uniform distribution. Hence, the hub-to-tip torsion of the blades is responsible for setting off a major spatial distortion between the rows. Complementarily, we observed that a reduction in the rows’ spacing or an increase in the blade loadings leads to a higher wake-blockage interaction, modifying the impingement of the incoming stator wakes. In addition, the deterministic stresses were calculated by time averaging the phase-dependent velocity correlations and compared to the turbulent stresses. The deterministic stresses were also segregated in temporal, spatial, and spatial-temporal correlations in order to analyze the dominant mechanisms involved in their generation. At this point, the deterministic kinetic energy levels were found to be generally lower than turbulent kinetic energy levels, with both temporal and spatial correlations being the most significant terms of the tensor.

1.
Adamczyk
,
J. J.
, 1986, “
Model Equation for Simulating Flows in Multistage Turbomachinery
,” ASME Paper No. 85-GT-226.
2.
Adamczyk
,
J. J.
, 2000, “
Aerodynamic Analysis of Multistage Turbomachinery Flows in Support of Aerodynamic Design
,”
ASME J. Turbomach.
0889-504X,
122
, pp.
189
217
.
3.
Meneveau
,
C.
, and
Katz
,
J.
, 2002, “
A Deterministic Stress Model for Rotor-Stator Interaction in Simulations of Average-Passage Flow
,”
ASME J. Fluids Eng.
0098-2202,
124
, pp.
550
554
.
4.
Uzol
,
O.
,
Chow
,
Y.-C.
,
Katz
,
J.
, and
Meneveau
,
C.
, 2002, “
Experimental Investigation of Unsteady Flow Field Within a Two-Stage Axial Turbomachine Using Particle Image Velocimetry
,”
ASME J. Turbomach.
0889-504X,
124
, pp.
542
552
.
5.
Chow
,
Y.-C.
,
Uzol
,
O.
, and
Katz
,
J.
, 2002, “
Flow Non-Uniformities and Turbulent “Hot Spots” Due to the Wake-Blade and Wake-Wake Interactions in a Multistage Turbomachine
,”
Proceedings of ASME Turbo Expo, 2002, Amsterdam
,
Netherlands
.
6.
Uzol
,
O.
,
Chow
,
Y.-C.
,
Katz
,
J.
, and
Meneveau
,
C.
, 2003, “
Average Passage Flow Field and Deterministic Stresses in the Tip and Hub Regions of a Multistage Turbomachine
,”
ASME J. Turbomach.
0889-504X,
125
, pp.
714
725
.
7.
Sinha
,
M.
,
Katz
,
J.
, and
Meneveau
,
C.
, 2000, “
Quantitative Visualization of the Flow in a Centrifugal Pump With Diffuser Vanes.—II: Addressing Passage-Averaged and Large-Eddy Simulation Modeling Issues in Turbomachinery Flows
,”
ASME J. Fluids Eng.
0098-2202,
122
, pp.
108
116
.
8.
Van de Wall
,
A. G.
,
Kadambi
,
J. R.
, and
Adamczyk
,
J. J.
, 2000, “
A Transport Model for the Deterministic Stresses Associated With Turbomachinery Blade Row Interactions
,”
ASME J. Turbomach.
0889-504X,
122
, pp.
593
603
.
9.
Van Zante
,
D. E.
,
Adamczyk
,
J. J.
,
Strazisar
,
A. J.
, and
Okiishi
,
T. H.
, 2002, “
Wake Recovery Performance Benefit in a High-Speed Axial Compressor
,”
ASME J. Turbomach.
0889-504X,
124
, pp.
275
284
.
10.
Adamczyk
,
J. J.
, 1996, “
Wake Mixing in Axial Flow Compressors
,” ASME Paper No. 96-GT-029.
11.
Kirtley
,
K. R.
, and
Beach
,
T. A.
, 1992, “
Deterministic Blade Row Interactions in a Centrifugal Compressor Stage
,”
ASME J. Turbomach.
0889-504X,
114
, pp.
304
311
.
12.
Adamczyk
,
J. J.
,
Beach
,
T. A.
,
Celestina
,
M. L.
,
Mulac
,
R. A.
, and
To
,
W. M.
, 1989, “
The Numerical Simulation of Multistage Turbomachinery Flows
,”
Proceedings of the AGARD Conference on Secondary Flows in Turbomachinery
.
13.
Chen
,
J. P.
,
Celestina
,
M. L.
, and
Adamczyk
,
J. J.
, 1994, “
A New Procedure for Simulating Unsteady Flows Through Turbomachinery Blade Passages
,” ASME Paper No. 94-GT-151.
14.
Leboeuf
,
F.
, 2002, “
Unsteady Flow Analysis in Transonic Turbine and Compressor Stages
,”
VKI Lecture Series
, 2002–01.
15.
Charbonnier
,
D.
, and
Leboeuf
,
F.
, 2005, “
Steady Flow Simulation of Rotor-Stator Interactions With an Unsteady Deterministic Model
,”
Proceedings of the Sixth European Conference on Turbomachinery
,
Lille
,
France
.
16.
Fernández Oro
,
J. M.
,
Argüelles Díaz
,
K. M.
,
Santolaria Morros
,
C.
, and
Blanco Marigorta
,
E.
, 2007, “
Unsteady Flow and Wake Transport in a Low-Speed Axial Fan With Inlet Guide Vanes
,”
ASME J. Fluids Eng.
0098-2202,
129
, pp.
1015
1029
.
17.
Blanco
,
E.
,
Ballesteros
,
R.
, and
Santolaria
,
C.
, 1998, “
Angular Range and Uncertainty Analysis of Non-Orthogonal Crossed Hot Wire Probes
,”
ASME J. Fluids Eng.
0098-2202,
123
, pp.
90
94
.
18.
Lyman
,
F. A.
, 1993, “
On the Conservation of Rothalpy in Turbomachines
,”
ASME J. Turbomach.
0889-504X,
115
, pp.
520
526
.
19.
Adamczyk
,
J. J.
,
Celestina
,
M. L.
,
Beach
,
T. A.
, and
Barnett
,
M.
, 1990, “
Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
,”
ASME J. Turbomach.
0889-504X,
112
, pp.
370
376
.
20.
Fernández Oro
,
J. M.
,
Argüelles Díaz
,
K. M.
,
Santolaria Morros
,
C.
, and
Ballesteros Tajadura
,
R.
, 2006, “
Upstream Potential Propagation Effects of Unsteady Rotor-Stator Interaction in an Axial Flow Blower
,” ASME-FEDSM-98244.
21.
Arnaud
,
D.
,
Ottavy
,
X.
, and
Vouillarmet
,
A.
, 2004, “
Experimental Investigation of the Rotor-Stator Interactions, Within a High Speed, Multi-Stage, Axial Compressor. Part 2—Modal Analysis of the Interactions
,” ASME Paper No. GT2004-53778.
22.
Fernández Oro
,
J. M.
, 2005, “
Unsteady Rotor-Stator Interaction in an Axial Turbomachine
,” Ph.D. thesis, University of Oviedo, Spain.
You do not currently have access to this content.