Abstract

This paper presents the simultaneous application of fast-response pressure transducers and unsteady pressure-sensitive paint (unsteady PSP) for the precise determination of pressure amplitudes and phases up to 3000 Hz. These experiments have been carried out on a low-pressure turbine blade cascade under engine-relevant conditions (Re, Ma, and Tu) in the high-speed cascade wind tunnel. Periodic blade/vane interactions were simulated at the inlet to the cascade using a wake generator operating at a constant perturbation frequency of 500 Hz. The main goal of this paper is the detailed comparison of amplitude and phase distributions between both flow sensing techniques at least up to the second harmonic of the wake generator’s fundamental perturbation frequency (i.e., 1000 Hz). Therefore, a careful assessment of the key drivers for relative deviations between measurement results as well as a detailed discussion of the data processing is presented for both measurement techniques. This discussion outlines the mandatory steps which were essential to achieve the quality as presented down to pressure amplitudes of several Pascal even under challenging experimental conditions. Apart from the remarkable consistency of the results, this paper reveals the potential of (unsteady) PSP as a future key flow sensing technique in turbomachinery research, especially for cascade testing. The results demonstrate that PSP was able to successfully sense pressure dynamics with very low fluctuation amplitudes down to 8 Pa.

References

1.
Sieverding
,
C. H.
,
Arts
,
T.
,
Dénos
,
R.
, and
Brouckaert
,
J.-F.
,
2000
, “
Measurement Techniques for Unsteady Flows in Turbomachines
,”
Exp. Fluids
,
28
(
4
), pp.
285
321
. 10.1007/s003480050390
2.
Ainsworth
,
R. W.
,
Dietz
,
A. J.
, and
Nunn
,
T. A.
,
1991
, “
The Use of Semi-Conductor Sensors for Blade Surface Pressure Measurement in a Model Turbine Stage
,”
ASME J. Eng. Gas Turbine Power
,
113
(
2
), pp.
261
268
. 10.1115/1.2906557
3.
Ainsworth
,
R. W.
,
Miller
,
R. J.
,
Moss
,
R. W.
, and
Thorpe
,
S. J.
,
2000
, “
Unsteady Pressure Measurement
,”
Meas. Sci. Technol.
,
11
(
7
), pp.
1055
1076
. 10.1088/0957-0233/11/7/319
4.
Engels-Putzka
,
A.
, and
Frey
,
C.
,
2015
, “
Adjoint Harmonic Balance Method for Forced Response Analysis in Turbomachinery
,”
6th International Conference on Computational Methods for Coupled Problems in Science and Engineering
,
Venice
,
May 18–20
, pp.
645
656
.
5.
Kulite Semiconductor Product Inc, 2019.
, “
Data Sheet LQ-062
,” http://www.kulitesensors.com.cn/pdf_Data_Sheets/LQ.LE-062.pdf, Accessed October 18, 2019.
6.
Vogt
,
D.
, and
Fransson
,
T.
,
2004
, “
A Technique for Using Recessed-Mounted Pressure Transducers to Measure Unsteady Pressure
,”
17th Symposium on Measuring Techniques in Transonic and Supersonic Flow in Cascades and Turbomachines, Stockholm
,
Sept. 9–10
,
NQC, Paper No. MTT1704-A514
.
7.
Engler
,
R. H.
,
Klein
,
C.
, and
Trinks
,
O.
,
2000
, “
Pressure Sensitive Paint Systems for Pressure Distribution Measurements in Wind Tunnels and Turbomachines
,”
Meas. Sci. Technol.
,
11
(
7
), pp.
1077
1085
. 10.1088/0957-0233/11/7/320
8.
Navarra
,
K. R.
,
Rabe
,
D. C.
,
Fonov
,
S. D.
,
Goss
,
L. P.
, and
Hah
,
C.
,
2000
, “
The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor
,”
ASME J. Turbomach.
,
123
(
4
), pp.
823
829
. 10.1115/1.1400116
9.
Lepicovsky
,
J.
, and
Bencic
,
T.
,
2002
, “
Use of Pressure-Sensitive Paint for Diagnostics in Turbomachinery Flows With Shocks
,”
Exp. Fluids
,
33
(
4
), pp.
531
538
. 10.1007/s00348-002-0476-x
10.
Niehuis
,
R.
, and
Bitter
,
M.
,
2021
, “
The High-Speed Cascade Wind Tunnel at the Bundeswehr University Munich After a Major Revision and Upgrade
,”
Proceedings of 14th European Conference on Turbomachinery Fluid dynamics and Thermodynamics
,
Gdansk
,
Apr. 12–16
,
Paper No. ETC2021-647
.
11.
Sturm
,
W.
, and
Fottner
,
L.
,
1985
, “
The High-Speed Cascade Wind-Tunnel of the German Armed Forces University Munich
,”
8th Symposium for Measurement Techniques in Transonic and Supersonic Flows in Cascades and Turbomachinery
,
Genoa
,
Oct. 24–25
,
Paper No. MTT0885-A102
.
12.
Acton
,
P.
,
Fottner
,
L.
, and
Fransson
,
T. H.
,
1998
,
Investigation of the Boundary Layer Development on a Highly Loaded Low Pressure Turbine Cascade Under the Influence of Unsteady Flow Conditions
,
Springer Dordrecht
, pp.
393
406
.
13.
Stieger
,
R. D.
, and
Hodson
,
H. P.
,
2005
, “
The Unsteady Development of a Turbulent Wake Through a Downstream Low-Pressure Turbine Blade Passage
,”
ASME J. Turbomach.
,
127
(
2
), pp.
388
394
. 10.1115/1.1811094
14.
Brunner
,
S.
, and
Fottner
,
L.
,
1999
, “
Untersuchungen zum Einfluß der Rotor-Stator Interaktion auf die saugseitige Transition eines hochbelasteten ungekühlten Niederdruck-Turbinengitters
,”
DGLR Jahrestagung, Berlin, Sept. 27–30, Paper No. DGLRJT99-078
.
15.
Bitter
,
M.
, and
Niehuis
,
R.
,
2019
, “
Effects of Periodic Inflow Turbulence on the Statistics in the Wake of a Linear LPT Cascade at Jet-Engine Relevant Test Conditions
,”
13th International Symposium on Particle Image Velocimetry–ISPIV 2019
,
Munich
,
July 22–24
.
16.
Hurst
,
A. M.
,
Olsen
,
T. R.
,
Goodman
,
S.
,
VanDeWeert
,
J.
, and
Shang
,
T.
,
2014
, “
An Experimental Frequency Response Characterization of MEMS Piezoresistive Pressure Transducers
,”
Proceedings of ASME Turbo Expo: Power for Land, Sea and Air
,
Paper No. GT2014-27159
.
17.
Bergh
,
H.
, and
Tijdeman
,
H.
,
1965
,
Theoretical and Experimental Results for the Dynamic Response of Pressure Measuring Systems
,
F.: Nationaal Lucht- en Ruimtevaartlaboratorium, Nationaal lucht- en ruimtevaartlaboratorium
.
18.
Bradshaw
,
P.
,
1971
,
An Introduction to Turbulence and Its Measurement
(
Thermodynamics and Fluid Mechanics Series
),
Pergamon Press
,
Oxford
.
19.
Gregory
,
J. W.
,
Asai
,
K.
,
Kameda
,
M.
,
Liu
,
T.
, and
Sullivan
,
J. P.
,
2008
, “
A Review of Pressure-Sensitive Paint for High-Speed and Unsteady Aerodynamics
,”
Proc. Inst. Mech. Eng. G-J. Aerosp. Eng.
,
222
(
2
), pp.
249
290
. 10.1243/09544100jaero243
20.
Wu
,
J.
,
Bitter
,
M.
,
Cai
,
G.
,
He
,
B.
, and
Kähler
,
C.
,
2017
, “
Investigation on Aerodynamic Force Effect of Vacuum Plumes Using Pressure-Sensitive Paint Technique and CFD-DSMC Solution
,”
Sci. China Technol. Sc.
,
60
(
7
), pp.
1058
1067
. 10.1007/s11431-016-9015-7
21.
Sugimoto
,
T.
,
Yorita
,
D.
,
Numata
,
D.
,
Nagai
,
H.
, and
Asai
,
K.
,
2011
, “
Evaluation of Transfer Function of Pressure-Sensitive Paint for Unsteady Flow Measurement
,”
11th Asian Symposium on Visualization
,
Niigata
,
June 5–9
.
22.
Liu
,
T.
, and
Sullivan
,
J. P.
,
2005
,
Pressure and Temperature Sensitive Paints
(
Experimental Fluid Mechanics
),
Springer-Verlag
,
Berlin
.
23.
McAuliffe
,
B. R.
, and
Yaras
,
M. I.
,
2009
, “
Transition Mechanisms in Separation Bubbles Under Low- and Elevated-Freestream Turbulence
,”
ASME J. Turbomach.
,
132
(
1
), p.
011004
. 10.1115/1.2812949
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