The effects of water ingestion on the performance of an axial flow compressor are experimentally studied with and without endwall treatment. The background to the work is derived from the assessment of airworthiness for an aero-engine. The stability-enhancing effects with endwall treatments under rain ingestion are not previously known. Moreover, all the endwall treatments are designed under dry air conditions in the compressor. Water ingestion at 3% and 5% relative to the design mass flow proposed in the airworthiness standard are applied to initially investigate the effects on the performance under smooth casing (SC). Results show that the water ingestions are mainly located near the casing wall after they move through the rotor blade row. The pressure rise coefficient increases, efficiency declines, and torque increases under the proposed water ingestion. The increase of the inlet water increases the thickness of the water film downstream the rotor blade row and aggravates the adverse effects on the performances. Subsequently, three endwall treatments, namely circumferential grooves, axial slots, and hybrid slots–grooves, are tested with and without water ingestion. Compared with no water ingestion, the circumferential grooves basically have no resistance to the water ingestion. The axial slots best prevent the drop of the pressure rise coefficient induced by water ingestion, and hybrid slots–grooves are the second-best place owing to the contribution of the front axial slots. Therefore, the hybrid slots–grooves can not only extend the stall margin with less efficiency penalty compared with axial slots, but also prevent rain ingestion from worsening the compressor performance.

References

1.
Kissel
,
G. J.
,
1980
, “
Rain and Hail Extremes at Altitude
,”
J. Aircr.
,
17
(
7
), pp.
464
467
.
2.
Devine
,
K.
,
1990
, “
Inclement Weather Induced Aircraft Engine Power Loss
,”
AIAA
Paper No. 90-2169.
3.
AGARD
,
1995
, “
Recommended Practices for the Assessment of the Effects of Atmospheric Water Ingestion on the Performance and Operability of Gas Turbine Engines
,” The Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France, Advisory Report No.
332
.https://www.scribd.com/document/60008150/AGARD-AR-332
4.
JAA
,
1997
, “
Ingestion of Rain and Hail, Harmonised Changes to JAR-E and FAR Part 33
,” Joint Aviation Authorities, Cologne, Germany, Technical Report.
5.
Riley
,
S.
,
1997
, “
Whole Engine Water/Ice Ingestion Strategy—Final Report
,” Rolls-Royce plc, Manchester, UK, Technical Report.
6.
Rolls-Royce plc
,
1996
,
The Jet Engine
, 5th ed.,
Rolls-Royce plc
, Manchester, UK.
7.
Davis
,
M.
,
2004
, “
A Numerical Investigation of the Effects of Steam Ingestion on Compression System Performance
,”
ASME
Paper No. GT2004-54190.
8.
Obermuller
,
M.
,
Schmidt
,
K.
,
Schulte
,
H.
, and
Peitsch
,
D.
,
2012
, “
Some Aspects on Wet Compression-Physical Effects and Modeling Strategies Used in Engine Performance Tools
,” Deutscher Luft- und Raumfahrtkongress, Berlin, Sept. 10–12, Paper No.
DLRK-2012-281210
.http://www.dglr.de/publikationen/2012/281210.pdf
9.
Venkataramani
,
K. S.
, and
McVey
,
L. J.
,
2006
, “
Scoop Effects in Inclement Weather Operation
,”
AIAA
Paper No. 2006-207.
10.
Day
,
I.
,
Williams
,
J.
, and
Freeman
,
C.
,
2008
, “
Rain Ingestion in Axial Flow Compressors at Part Speed
,”
ASME J. Turbomach.
,
130
(
1
), p.
011024
.
11.
Williams
,
J.
,
2008
, “
Further Effects of Water Ingestion on Axial Flow Compressors and Aeroengines at Part Speed
,”
ASME
Paper No. GT2008-50620.
12.
Roumeliotis
,
I.
,
Alexiou
,
A.
,
Aretakis
,
N.
,
Sieros
,
G.
, and
Mathioudakis
,
K.
,
2014
, “
Development and Integration of Rain Ingestion Effects in Engine Performance Simulations
,”
ASME J. Eng. Gas Turbines Power
,
137
(
4
), p.
041202
.
13.
Liu
,
L.
,
Zhang
,
H.
,
Li
,
J.
,
Yu
,
C.
,
Lin
,
F.
, and
Nie
,
C.
,
2013
, “
Measurements and Visualization of Process From Steady-State to Stall in an Axial Compressor With Water Ingestion
,”
ASME
Paper No. GT2013-95253.
14.
Eisfeld
,
T.
, and
Joos
,
F.
,
2009
, “
Experimental Investigation of Two-Phase Flow Phenomena in Transonic Compressor Cascades
,”
ASME
Paper No. GT2009-59365.
15.
Das
,
K.
,
Hamed
,
A. A.
, and
Basu
,
D.
,
2006
, “
Droplet Trajectories and Collection on Fan Rotor at Off-Design Conditions
,”
ASME
Paper No. GT2006-91214.
16.
Nikolaidis
,
T.
,
Pilidis
,
P.
,
Teixeira
,
J. A.
, and
Pachidis
,
V.
,
2008
, “
Water Film Formation on an Axial Flow Compressor Rotor Blade
,”
ASME
Paper No. GT2008-50137.
17.
Hathaway
,
M. D.
,
2007
, “
Passive Endwall Treatments for Enhancing Stability
,” National Aeronautics and Space Administration, Cleveland, OH, Report No.
TM-2007-214409
.https://ntrs.nasa.gov/search.jsp?R=20070025023
18.
Day
,
I. J.
,
1993
, “
Active Suppression of Rotating Stall and Surge in Axial Compressors
,”
ASME J. Turbomach.
,
115
(
1
), pp.
40
47
.
19.
Li
,
J.
,
2016
, “
Self-Adaptive Stability-Enhancing Technology With Tip Air Injection in an Axial Flow Compressor
,”
ASME J. Turbomach.
,
139
(
1
), p.
011008
.
20.
Geng, S., Zhang, H., Chen, J., and Huang, W., 2007, “
Numerical Study on the Unsteady Response of Tip Leakage Flow Unsteadiness to Discrete Micro Tip Injection in a Low-Speed Isolated Compressor
,”
ASME
Paper No. GT2007-27729.
21.
Du
,
J.
,
Li
,
J.
,
Gao
,
L.
,
Lin
,
F.
, and
Chen
,
J.
,
2016
, “
The Impact of Casing Groove Location on Stall Margin and Tip Clearance Flow in a Low-Speed Axial Compressor
,”
ASME J. Turbomach.
,
138
(
12
), p.
121007
.
22.
Du
,
J.
,
Li
,
F.
,
Li
,
J.
,
Ma
,
N.
,
Lin
,
F.
, and
Chen
,
J.
,
2015
, “
A Study of Performance and Flow Mechanism of a Slot-Groove Hybrid Casing Treatment in a Low-Speed Compressor
,”
ASME
Paper No. GT2015-43920.
23.
Qingxiang
,
M.
,
2002
, “
Aero Engine Sea Level Water Ingestion Simulation Test
,”
J. Gas Turbine Exp. Res.
,
15
(
4
), pp.
39
44
(in Chinese).
24.
Houghton
,
T.
, and
Day
,
I.
,
2010
, “
Enhancing the Stability of the Subsonic Compressor Using Casing Grooves
,”
ASME J. Turbomach.
,
133
(
2
), p.
021007
.
25.
Li
,
J.
,
Lin
,
F.
,
Wang
,
S.
,
Du
,
J.
,
Nie
,
C.
, and
Chen
,
J.
,
2014
, “
Extensive Experimental Study of Circumferential Single Groove in an Axial Flow Compressor
,”
ASME
Paper No. GT2014-26859.
26.
Li
,
J.
,
Lin
,
F.
,
Tong
,
Z.
,
Nie
,
C.
, and
Chen
,
J.
,
2015
, “
The Dual Mechanisms and Implementations of Stability Enhancement With Discrete Tip Injection in Axial Flow Compressors
,”
ASME J. Turbomach.
,
137
(
3
), p.
031010
.
27.
Zhang
,
H.
,
Tian
,
X.
,
Pan
,
X.
,
Zhou
,
J.
, and
Zheng
,
Q.
,
2016
, “
Formation Process of Water Film and Performance Effect on Compressor Stage
,”
ASME
Paper No. GT2016-56569.
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