Accuracy when assessing mistuned forced response analyses is still a major concern. Since a fully coupled analysis is still very computational expensive, several simplifications and reduced-order models (ROMs) are carried out. The use of a reduction method, the assumptions and simplifications, generate different uncertainties that challenge the accuracy of the results. Experimental data are needed for validation and also to understand the propagation of these uncertainties. This paper shows a detailed mistuned forced response analysis of a compressor blisk. The blisk belongs to the Purdue Three-Stage (P3S) Compressor Research Facility. Two different stator–rotor–stator configurations of 38 and 44 upstream stator vanes are taken into consideration. Several loading conditions are analyzed at three different speed lines. A ROM known as subset nominal mode (SNM), has been used for all the analyses. This reduction takes as a basis a set of modes within a selected frequency spectrum. It can consider a complete family of modes to study the disk–blade modal interaction. A detailed comparison between the predicted and measured results has been performed, showing a good agreement for the high loading (HL) conditions.

References

1.
Craig
,
R. R.
, and
Bampton
,
M. C. C.
,
1968
, “
Coupling of Substructures for Dynamic Analyses
,”
AIAA J.
,
6
(
7
), pp.
1313
1319
.
2.
Bladh
,
R.
,
Castanier
,
M. P.
, and
Pierre
,
C.
,
2000
, “
Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks-Part I: Theoretical Models
,”
ASME J. Eng. Gas Turbines Power
,
123
(
1
), pp.
89
99
.
3.
Moyroud
,
F.
,
Fransson
,
T.
, and
Jacquet-Richardet
,
G.
,
2002
, “
A Comparison of Two Finite Element Reduction Techniques for Mistuned Bladed Disks
,”
ASME J. Eng. Gas Turbines Power
,
124
(
4
), pp.
942
952
.
4.
Lim
,
S.-H.
,
Bladh
,
R.
, and
Castanier
,
M. P.
,
2007
, “
Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
,”
AIAA J.
,
45
(
9
), pp.
2285
2298
.
5.
Yang
,
M.-T.
, and
Griffin
,
J.
,
2001
, “
A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes
,”
ASME J. Eng. Gas Turbines Power
,
123
(
4
), pp.
893
900
.
6.
Feiner
,
D.
, and
Griffin
,
J.
,
2002
, “
A Fundamental Model of Mistuning for a Single Family of Modes
,”
ASME J. Turbomach.
,
124
(
4
), pp.
597
605
.
7.
Martel
,
C.
,
Corral
,
R.
, and
Llorens
,
J. M.
,
2008
, “
Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
,”
ASME J. Turbomach.
,
130
(
1
), p.
011006
.
8.
Gutierrez Salas
,
M.
,
Bladh
,
R.
,
Mårtensson
,
H.
,
Petrie-Repar
,
P.
,
Fransson
,
T.
, and
Vogt
,
D. M.
,
2017
, “
Forced Response Analysis of a Mistuned, Compressor Blisk Comparing Three Different Reduced Order Model Approaches
,”
ASME J. Eng. Gas Turbines Power
,
139
(
6
), p.
062501
.
9.
Besem
,
F. M.
,
Kielb
,
R. E.
,
Galpin
,
P.
,
Zori
,
L.
, and
Key
,
N. L.
,
2016
, “
Mistuned Forced Response Predictions of an Embedded Rotor in a Multistage Compressor
,”
ASME J. Turbomach.
,
138
(
6
), p.
061003
.
10.
Li
,
J.
,
Aye-Addo
,
N.
,
Kormanik
,
N.
, III
,
Matthews
,
D.
,
Key
,
N.
, and
Kielb
,
R.
,
2017
, “
Mistuned Higher-Order Mode Forced Response of an Embedded Compressor Rotor, Part I: Steady and Unsteady Aerodynamics
,”
ASME
Paper No. GT2017-64633.
11.
Li
,
J.
,
Aye-Addo
,
N.
,
Kielb
,
R.
, and
Key
,
N.
,
2017
, “
Mistuned Higher-Order Mode Forced Response of an Embedded Compressor Rotor, Part II: Mistuned Forced Response Prediction
,”
ASME J. Turbomach.
,
140
(
3
), p.
031006
.
12.
Castanier
,
M. P.
,
Ottarsson
,
G.
, and
Pierre
,
C.
,
1997
, “
A Reduced Order Modeling Technique for Mistuned Bladed Disks
,”
ASME J. Vib. Acoust.
,
119
(
3
), pp.
439
447
.
13.
Whitehead
,
D. S.
,
1966
, “
Effect of Mistuning on the Vibration of Turbomachine Blades Induced by Wakes
,”
J. Mech. Eng. Sci.
,
8
(
1
), pp.
15
21
.
You do not currently have access to this content.