Careful experimental measurements can capture small changes in compressor total pressure ratio (TPR), which arise with subtle changes in an experiment's configuration. Research facilities that use unconditioned atmospheric air must account for changes in ambient compressor inlet conditions to establish repeatable performance maps. A unique dataset from a three-stage axial compressor has been acquired over the duration of 12 months in the Midwest U.S., where ambient conditions change significantly. The trends show a difference in compressor TPR measured on a cold day versus a warm day despite correcting inlet conditions to sea level standard day. To reconcile these differences, this paper explores correcting the compressor exit thermodynamic state, Reynolds number effects, and variations in rotor tip clearance (TC) as a result of differences in thermal growth.

References

1.
Cumpsty
,
N. A.
,
2004
,
Compressor Aerodynamics
,
Krieger
,
Malabar, FL
, pp.
11
21
.
2.
Dixon
,
S. L.
,
2005
,
Fluid Mechanics and Thermodynamics of Turbomachinery
,
Elsevier
,
Burlington, MA
, pp.
16
20
.
3.
Fishbeyn
,
B. D.
, and
Pervyshin
,
N. V.
,
1970
, “
Determination of the Effect of Atmospheric Humidity on the Characteristics of a Turbofan Engine
,” Foreign Technology Division, Wright-Patterson AFB, OH, Paper No. FTD-HT-23-290-68.
4.
Bird
,
J.
, and
Grabe
,
W.
,
1991
, “
Humidity Effects on Gas Turbine Performance
,”
International Gas Turbine and Aeroengine Congress and Exposition
,
Orlando, FL
, June 3–6,
ASME
Paper No. 91-GT-329.
5.
Berdanier
,
R. A.
,
Smith
,
N. R.
,
Fabian
,
J. C.
, and
Key
,
N. L.
,
2015
, “
Humidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases
,”
ASME J. Turbomach.
,
137
(
3
), p.
031011
.
6.
American Society of Mechanical Engineers
,
1997
, “
Performance Test Code on Compressors and Exhausters
,” ASME, New York, ASME Standard No. PTC 10.
7.
Wiesner
,
F. J.
,
1979
, “
A New Appraisal of Reynolds Number Effects on Centrifugal Compressor Performance
,”
ASME J. Eng. Power
,
101
(
3
), pp.
384
392
.
8.
Strub
,
R. A.
,
Bonciani
,
L.
,
Borer
,
C. J.
,
Casey
,
M. V.
,
Cole
,
S. L.
,
Cook
,
B. B.
,
Kotzur
,
J.
,
Simon
,
H.
, and
Strite
,
M. A.
,
1987
, “
Influence of the Reynolds Number on the Performance of Centrifugal Compressors
,”
ASME J. Turbomach.
,
109
(
4
), pp.
541
544
.
9.
Carter
,
A. D. S.
,
Moss
,
C. E.
,
Green
,
G. R.
, and
Annear
,
G. G.
,
1957
, “
The Effect of Reynolds Number on the Performance of a Single-Stage Compressor
,” Ministry of Aviation, Aeronautical Research Council, London, Reports and Memoranda No. 3184.
10.
Wassel
,
A. B.
,
1968
, “
Reynolds Number Effects in Axial Compressors
,”
ASME J. Eng. Power
,
90
(
2
), pp.
149
156
.
11.
Schäffler
,
A.
,
1980
, “
Experimental and Analytical Investigation of the Effects of Reynolds Number and Blade Surface Roughness on Multistage Axial Flow Compressors
,”
ASME J. Eng. Power
,
102
(
1
), pp.
5
12
.
12.
Walsh
,
P. P.
, and
Fletcher
,
P.
,
2008
,
Gas Turbine Performance
,
Blackwell Science
,
Oxford, UK
, p.
149, 168, 407
.
13.
Shepherd
,
D. G.
,
1956
,
Principles of Turbomachinery
,
Macmillan
,
New York
, pp.
39
47
.
14.
Jefferson
,
J. L.
, and
Turner
,
R. C.
,
1958
, “
Some Shrouding and Tip Clearance Effects in Axial Flow Compressors
,”
Int. Shipbuild. Prog.
,
5
(
42
), pp.
78
101
.
15.
Wisler
,
D. C.
,
1985
, “
Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing
,”
ASME J. Eng. Gas. Turbine Power
,
107
(
2
), pp.
354
363
.
16.
Freeman
,
C.
,
1985
, “
Effect of Tip Clearance Flow on Compressor Stability and Engine Performance
” (VKI Lecture Series 1985-05), von Karman Institute, Rhode-St-Genese, Belgium.
17.
Tschirner
,
T.
,
Johann
,
E.
,
Müller
,
R.
, and
Vogeler
,
K.
,
2006
, “
Effects of 3D Aerofoil Tip Clearance Variation on a 4-Stage Low Speed Compressor
,”
ASME
Paper No. GT2006-90902.
18.
Wright
,
J. D.
,
2010
, “
Properties for Accurate Gas Flow Measurements
,”
15th Flow Measurement Conference (FLOMEKO)
,
Taipei, Taiwan
, Oct. 13–15.
19.
Lemmon
,
E. W.
,
Huber
,
M. L.
, and
McLinden
,
M. O.
,
2013
, “
NIST Standard Reference Database 23: Reference Fluid Thermodynamic and Transport Properties—refprop, Version 9.1
,” National Institute of Standards and Technology, Standard Reference Data Program, Gaithersburg, MD.
20.
Wexler
,
A.
,
1976
, “
Vapor Pressure Formulation for Water in Range 0 to 100 °C. A Revision
,”
J. Res. Natl. Bur. Stand.
,
80A
(
5
), pp.
775
785
.
21.
Wexler
,
A.
,
1977
, “
Vapor Pressure Formulation for Ice
,”
J. Res. Natl. Bur. Stand.
,
81A
(
1
), pp.
5
20
.
22.
WMO
,
1966
,
International Meteorological Tables
,
S.
Letestu
, ed.,
World Meterological Organization
,
Geneva
, Report No. 188 TP 94, Table 4.3, pp.
3
4
.
23.
Smith
,
L. H.
,
1964
, “
Some Comments on Reynolds Number
,”
ASME J. Eng. Power
,
86
(
3
), pp.
225
226
.
24.
American Society of Mechanical Engineers
, 2004, “
Flow Measurement
,” ASME, New York, ASME Standard No. PTC 19.5, pp.
19
27
.
25.
Berdanier
,
R. A.
, and
Key
,
N. L.
,
2015
, “
Experimental Investigation of Factors Influencing Operating Rotor Tip Clearance in Multistage Compressors
,”
Int. J. Rotating Mach.
,
2015
, p.
146272
.
26.
Johnsen
,
I. A.
, and
Bullock
,
R. O.
, eds.,
1965
,
Aerodynamic Design of Axial-Flow Compressors
,
NASA
,
Washington, DC
, p.
206
.
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