-
1
-
-
0001759524
-
Flutter and Resonant Vibration Characteristics of Engine Blades
-
10.1115/1.2817053
-
Srinivasan A. Flutter and Resonant Vibration Characteristics of Engine Blades. ASME J. Eng. Gas Turbines Power 1997, 119:742-775. 10.1115/1.2817053
-
(1997)
ASME J. Eng. Gas Turbines Power
, vol.119
, pp. 742-775
-
-
Srinivasan, A.1
-
2
-
-
0029673651
-
A Review of Aeroelasticity Methods With Emphasis on Turbomachinery Applications
-
10.1006/jfls.1996.0015
-
Marshall J. Imregun M. A Review of Aeroelasticity Methods With Emphasis on Turbomachinery Applications. J. Fluids Struct. 1996, 10:237-267. 10.1006/jfls.1996.0015
-
(1996)
J. Fluids Struct.
, vol.10
, pp. 237-267
-
-
Marshall, J.1
Imregun, M.2
-
3
-
-
30744456273
-
Recent Advancements in Turbomachinery Aeroelastic Analysis
-
Reno, Nevada, AIAA Paper No. 2055-0014.
-
Hall K. Kielb R. Ekici K. Thomas J. Recent Advancements in Turbomachinery Aeroelastic Analysis. Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit 2005, and "," Reno, Nevada, AIAA Paper No. 2055-0014.
-
(2005)
Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit
-
-
Hall, K.1
Kielb, R.2
Ekici, K.3
Thomas, J.4
-
5
-
-
0032182653
-
Whole-Assembly Flutter Analysis of a Low-Pressure Turbine Blade
-
10.1007/978-94-011-5040-8
-
Sayma A. Vahdati M. Green J. Imregun M. Whole-Assembly Flutter Analysis of a Low-Pressure Turbine Blade. Aeronaut. J. 1998, 102:459-463. 10.1007/978-94-011-5040-8
-
(1998)
Aeronaut. J.
, vol.102
, pp. 459-463
-
-
Sayma, A.1
Vahdati, M.2
Green, J.3
Imregun, M.4
-
6
-
-
0033812197
-
Flutter Mechanisms in Low Pressure Turbine Blades
-
10.1115/1.483179
-
Nowinski M. Panovsky J. Flutter Mechanisms in Low Pressure Turbine Blades. J. Eng. Gas Turbines Power 2000, 122:89-98. 10.1115/1.483179
-
(2000)
J. Eng. Gas Turbines Power
, vol.122
, pp. 89-98
-
-
Nowinski, M.1
Panovsky, J.2
-
7
-
-
77955258320
-
Identification of the Stability Margin Between Safe Operation and the Onset of Blade Flutter
-
10.1115/1.2812339
-
Rice T. Bell D. Singh G. Identification of the Stability Margin Between Safe Operation and the Onset of Blade Flutter. ASME J. Turbomach. 2009, 131:011009. 10.1115/1.2812339
-
(2009)
ASME J. Turbomach.
, vol.131
, pp. 011009
-
-
Rice, T.1
Bell, D.2
Singh, G.3
-
8
-
-
4944236955
-
Stabilization of Linear Flow Solver for Turbomachinery Aeroelasticity Using Recursive Projection Method
-
10.2514/1.1225
-
Campobasso M. Giles M. Stabilization of Linear Flow Solver for Turbomachinery Aeroelasticity Using Recursive Projection Method. AIAA J. 2004, 42(9):1765-1774. 10.2514/1.1225
-
(2004)
AIAA J.
, vol.42
, Issue.9
, pp. 1765-1774
-
-
Campobasso, M.1
Giles, M.2
-
9
-
-
0033822152
-
A Design Method to Prevent Low Pressure Turbine Blade Flutter
-
10.1115/1.483180
-
Panovsky J. Kielb R. A Design Method to Prevent Low Pressure Turbine Blade Flutter. Trans. ASME: J. Eng. Gas Turbines and Power 2000, 122:89-98. 10.1115/1.483180
-
(2000)
Trans. ASME: J. Eng. Gas Turbines and Power
, vol.122
, pp. 89-98
-
-
Panovsky, J.1
Kielb, R.2
-
10
-
-
34547102734
-
3-D Inviscid Self-Excited Vibrations of a Blade Row in the Last Stage Turbine
-
10.1016/j.jfluidstructs.2006.12.003
-
Rzadkowski R. Gnesin V. 3-D Inviscid Self-Excited Vibrations of a Blade Row in the Last Stage Turbine. J. Fluids Struct. 2007, 23:858-873. 10.1016/j.jfluidstructs.2006.12.003
-
(2007)
J. Fluids Struct.
, vol.23
, pp. 858-873
-
-
Rzadkowski, R.1
Gnesin, V.2
-
11
-
-
0021199602
-
Effects of Structural Coupling on Mistuned Cascade Flutter and Response
-
10.1115/1.3239532
-
Kielb R.E. Kaza K.R. V. Effects of Structural Coupling on Mistuned Cascade Flutter and Response. Trans. ASME: J. Eng. Gas Turbines Power 1984, 106:17-24. 10.1115/1.3239532
-
(1984)
Trans. ASME: J. Eng. Gas Turbines Power
, vol.106
, pp. 17-24
-
-
Kielb, R.E.1
Kaza, K.R.V.2
-
12
-
-
0022792144
-
The Effect of Circumferential Aerodynamic Detuning on Coupled Bending-Torsional Unstalled Supersonic Flutter
-
10.1115/1.3262045
-
Hoyniak D. Fleeter S. The Effect of Circumferential Aerodynamic Detuning on Coupled Bending-Torsional Unstalled Supersonic Flutter. ASME J. Turbomach. 1986, 108:253-260. 10.1115/1.3262045
-
(1986)
ASME J. Turbomach.
, vol.108
, pp. 253-260
-
-
Hoyniak, D.1
Fleeter, S.2
-
13
-
-
47649089993
-
Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
-
10.1115/1.2720503
-
Martel C. Corral R. Llorens J.M. Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning. ASME J. Turbomach. 2008, 130:011006. 10.1115/1.2720503
-
(2008)
ASME J. Turbomach.
, vol.130
, pp. 011006
-
-
Martel, C.1
Corral, R.2
Llorens, J.M.3
-
14
-
-
10244276930
-
Flutter of Mistuned Bladed Disks and Blisks With Aerodynamic and FMM Structural Coupling
-
Vienna, Austria, Paper No. GT2004-54315.
-
Kielb R. Feiner D. Griffin J. Miyakozawa T. Flutter of Mistuned Bladed Disks and Blisks With Aerodynamic and FMM Structural Coupling. Proceedings of ASME Turbo Expo 2004 2004, and "," Vienna, Austria, Paper No. GT2004-54315.
-
(2004)
Proceedings of ASME Turbo Expo 2004
-
-
Kielb, R.1
Feiner, D.2
Griffin, J.3
Miyakozawa, T.4
-
15
-
-
77955256420
-
Aeroelastic Analysis of Rotors With Flexible Disks and Alternate Blade Mistuning
-
10.1115/1.2812957, and "" p.
-
Bleeg J. Yang M.-T. Eley J. Aeroelastic Analysis of Rotors With Flexible Disks and Alternate Blade Mistuning. ASME J. Turbomach. 2009, 131:011011. 10.1115/1.2812957, and "" p.
-
(2009)
ASME J. Turbomach.
, vol.131
, pp. 011011
-
-
Bleeg, J.1
Yang, M.-T.2
Eley, J.3
-
16
-
-
0020737330
-
Friction Damping of Flutter in Gas Turbine Engine Airfoils
-
10.2514/3.44878
-
Sinha A. Griffin J. Friction Damping of Flutter in Gas Turbine Engine Airfoils. J. Aircr. 1983, 20(4):372-376. 10.2514/3.44878
-
(1983)
J. Aircr.
, vol.20
, Issue.4
, pp. 372-376
-
-
Sinha, A.1
Griffin, J.2
-
17
-
-
0022011349
-
Effects of Friction Dampers on Aerodynamically Unstable Rotor Stages
-
10.2514/3.8904
-
Sinha A. Griffin J. Effects of Friction Dampers on Aerodynamically Unstable Rotor Stages. AIAA J. 1985, 23(2):262-270. 10.2514/3.8904
-
(1985)
AIAA J.
, vol.23
, Issue.2
, pp. 262-270
-
-
Sinha, A.1
Griffin, J.2
-
18
-
-
33750796649
-
A Methodology for the Vibration Amplitude Prediction of Self-Excited Rotors Based on Dimensional Analysis
-
Barcelona, Spain, Paper No. GT2006-90668.
-
Corral R. Gallardo J. A Methodology for the Vibration Amplitude Prediction of Self-Excited Rotors Based on Dimensional Analysis. Proceedings of ASME Turbo Expo 2006, and "," Barcelona, Spain, Paper No. GT2006-90668.
-
(2006)
Proceedings of ASME Turbo Expo
-
-
Corral, R.1
Gallardo, J.2
-
19
-
-
0032714258
-
Suppression of Bending-Torsion Flutter Through Displacement-Dependent Dry Friction Damping
-
10.2514/2.667
-
Whiteman W. Ferri A. Suppression of Bending-Torsion Flutter Through Displacement-Dependent Dry Friction Damping. AIAA J. 1999, 37(1):79-83. 10.2514/2.667
-
(1999)
AIAA J.
, vol.37
, Issue.1
, pp. 79-83
-
-
Whiteman, W.1
Ferri, A.2
-
20
-
-
10944257546
-
Modeling Viscous Transonic Limit-Cycle Oscillation Behavior Using a Harmonic Balance Approach
-
10.2514/1.9839
-
Thomas J. Dowell E. Hall K. Modeling Viscous Transonic Limit-Cycle Oscillation Behavior Using a Harmonic Balance Approach. J. Aircr. 2004, v.41:1266-1274. 10.2514/1.9839
-
(2004)
J. Aircr.
, vol.v.41
, pp. 1266-1274
-
-
Thomas, J.1
Dowell, E.2
Hall, K.3
-
21
-
-
34047163427
-
A High Dimensional Harmonic Balance Approach for an Aeroelastic Airfoil With Cubic Restoring Forces
-
10.1016/j.jfluidstructs.2006.09.005
-
Liu L. Dowell E. Thomas J. A High Dimensional Harmonic Balance Approach for an Aeroelastic Airfoil With Cubic Restoring Forces. J. Fluids Struct. 2007, 23:351-363. 10.1016/j.jfluidstructs.2006.09.005
-
(2007)
J. Fluids Struct.
, vol.23
, pp. 351-363
-
-
Liu, L.1
Dowell, E.2
Thomas, J.3
-
22
-
-
82055184845
-
Nonlinear Flutter in Fan Stator Vanes With Time Dependent Fixity
-
Glasgow, UK, June 14-18, Paper No. GT2010-22555.
-
Srivastava R. Panovsky J. Kileb R. Virgin L. Ekici K. Nonlinear Flutter in Fan Stator Vanes With Time Dependent Fixity. Proceedings of ASME Turbo Expo 2010 2010, and "," Glasgow, UK, June 14-18, Paper No. GT2010-22555.
-
(2010)
Proceedings of ASME Turbo Expo 2010
-
-
Srivastava, R.1
Panovsky, J.2
Kileb, R.3
Virgin, L.4
Ekici, K.5
-
23
-
-
0037978988
-
Analytical Formulation of Friction Interface Elements for Analysis of Nonlinear Multi-Harmonic Vibrations of Bladed Discs
-
10.1115/1.1539868
-
Petrov E.P. Ewins D.J. Analytical Formulation of Friction Interface Elements for Analysis of Nonlinear Multi-Harmonic Vibrations of Bladed Discs. ASME J. Turbomach. 2003, 125:364-371. 10.1115/1.1539868
-
(2003)
ASME J. Turbomach.
, vol.125
, pp. 364-371
-
-
Petrov, E.P.1
Ewins, D.J.2
-
24
-
-
1942521159
-
A Method for Use of Cyclic Symmetry Properties in Analysis of Nonlinear Multiharmonic Vibrations of Bladed Discs
-
10.1115/1.1644558
-
Petrov E.P. A Method for Use of Cyclic Symmetry Properties in Analysis of Nonlinear Multiharmonic Vibrations of Bladed Discs. ASME J. Turbomach. 2004, 126:175-183. 10.1115/1.1644558
-
(2004)
ASME J. Turbomach.
, vol.126
, pp. 175-183
-
-
Petrov, E.P.1
-
25
-
-
33745233094
-
Effects of Damping and Varying Contact Area at Blade-Disc Joints in Forced Response Analysis of Bladed Disc Assemblies
-
10.1115/1.2181998
-
Petrov E.P. Ewins D.J. Effects of Damping and Varying Contact Area at Blade-Disc Joints in Forced Response Analysis of Bladed Disc Assemblies. ASME J. Turbomach. 2006, 128:403-410. 10.1115/1.2181998
-
(2006)
ASME J. Turbomach.
, vol.128
, pp. 403-410
-
-
Petrov, E.P.1
Ewins, D.J.2
-
26
-
-
78149374016
-
A Method for Forced Response Analysis of Mistuned Bladed Discs With Aerodynamic Effects Included
-
10.1115/1.4000117
-
Petrov E. A Method for Forced Response Analysis of Mistuned Bladed Discs With Aerodynamic Effects Included. Trans. ASME: J. Eng. Gas Turbines Power 2010, 132:062502. 10.1115/1.4000117
-
(2010)
Trans. ASME: J. Eng. Gas Turbines Power
, vol.132
, pp. 062502
-
-
Petrov, E.1
-
27
-
-
34548241151
-
Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Discs
-
10.1115/1.2720487
-
Petrov E.P. Direct Parametric Analysis of Resonance Regimes for Nonlinear Vibrations of Bladed Discs. ASME J. Turbomach. 2007, 129:495-502. 10.1115/1.2720487
-
(2007)
ASME J. Turbomach.
, vol.129
, pp. 495-502
-
-
Petrov, E.P.1
-
28
-
-
78149379712
-
Method for Sensitivity Analysis of Resonance Forced Response of Bladed Disks With Nonlinear Contact Interfaces
-
10.1115/1.2969094
-
Petrov E.P. Method for Sensitivity Analysis of Resonance Forced Response of Bladed Disks With Nonlinear Contact Interfaces. Trans. ASME: J. Eng. Gas Turbines Power 2009, 131:022510. 10.1115/1.2969094
-
(2009)
Trans. ASME: J. Eng. Gas Turbines Power
, vol.131
, pp. 022510
-
-
Petrov, E.P.1
-
29
-
-
0033729894
-
Modeling of Three-Dimensional Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids
-
10.2514/2.1062
-
Sayma A. Vahdati M. Sbardella L. Imregun M. Modeling of Three-Dimensional Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids. AIAA J. 2000, 38(6):945-954. 10.2514/2.1062
-
(2000)
AIAA J.
, vol.38
, Issue.6
, pp. 945-954
-
-
Sayma, A.1
Vahdati, M.2
Sbardella, L.3
Imregun, M.4
-
30
-
-
79957650658
-
A High-Accuracy Model Reduction for Analysis of Nonlinear Vibrations in Structures With Contact Interfaces
-
10.1115/1.4002810
-
Petrov E.P. A High-Accuracy Model Reduction for Analysis of Nonlinear Vibrations in Structures With Contact Interfaces. Trans. ASME: J. Eng. Gas Turbines Power 2011, 133:102503. 10.1115/1.4002810
-
(2011)
Trans. ASME: J. Eng. Gas Turbines Power
, vol.133
, pp. 102503
-
-
Petrov, E.P.1
|