Open Access
Issue
JNWPU
Volume 36, Number 5, October 2018
Page(s) 856 - 864
DOI https://doi.org/10.1051/jnwpu/20183650856
Published online 17 December 2018
  1. Kielb R E, Hall K C, Hong E, et al. Probabilistic Flutter Analysis of a Mistuned Bladed Disk[R]. GT2006-90847 [Google Scholar]
  2. Martel C, Corral R, Llorens J M. Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning[J]. Journal of Turbomachinery, 2008, 130(1): 1045-1058 [Article] [CrossRef] [Google Scholar]
  3. Campobasso M S, Giles M B. Analysis of the Effect of Mistuning on Turbomachinery Aeroelasticity[C]//Proceedings of the IX Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity in Turbomachines, 2001 [Google Scholar]
  4. Whitehead D S. Effect of Mistuning on the Vibration of Turbo-Machine Blades Induced by Wakes[J]. Journal of Mechanical Engineering Science, 1966, 8(1): 15-21 [Article] [CrossRef] [Google Scholar]
  5. Dye R C F, Henry T A. Vibration Amplitudes of Compressor Blades Resulting from Scatter in Blade Natural Frequencies[J]. ASME Journal of Engineering for Power, 1969, 91(7): 182-188 [Article] [CrossRef] [Google Scholar]
  6. Kaza K R V, Kielb R E. Flutter and Response of a Mistuned Cascade in Incompressible Flow[J]. AIAA Journal, 1982, 20(8): 1120-1127 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  7. Pierre C, Murthy D. Aeroelastic Model Characteristics of Mistuned Blade Assemblies:Mode Localization and Loss of Eigenstructure[J]. AIAA Journal, 1992, 30(10): 2483-2496 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  8. Pierre C, Smith T E, Murthy D. Localization of Aeroelastic Modes in Mistuned High-Energy Turbines[J]. Journal of Propulsion and Power, 1994, 10(3): 318-328 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  9. Bladh R, Pierre C, Castanier M P, et al. Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced-Order Modeling[J]. Journal of Engineering for Gas Turbines and Power, 2002, 124(2): 311-324 [Article] [CrossRef] [Google Scholar]
  10. Judge J, Pierre C, Mehmed O. Experimental Investigation of Mode Localization and Forced Response Amplitude Magnification for a Mistuned Bladed Disk[J]. Journal of Engineering for Gas Turbines and Power, 2001, 123(4): 940-950 [Article] [CrossRef] [Google Scholar]
  11. Saito A, Castanier M P, Pierre C. Effects of a Cracked Blade on Mistuned Turbine Engine Rotor Vibration[J]. Journal of Vibration and Acoustics, 2009, 131(12): 1-9 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  12. Song S H, Castanier M P, Pierre C. System Identification of Multistage Turbine Engine Rotors[C]//ASME Turbo Expo 2007: Power for Land, Sea and Air, 2007: 569-582 [Google Scholar]
  13. Petrov E P, Sanliturk K Y, Ewins D J. A New Method for Dynamic Analysis of Mistuned Bladed Disks Based on the Exact Relationship between Tuned and Mistuned Systems[J]. Journal of Engineering for Gas Turbines and Power, 2002, 124(3): 586-597 [Article] [CrossRef] [Google Scholar]
  14. Petrov E P, Ew ins D J. Analysis of the Worst Mistuning Patterns in Bladed Disk Assemblies[J]. Journal of Turbomchinery, 2003, 125(4): 623-631 [Article] [CrossRef] [Google Scholar]
  15. Petrov E P. Reduction of Forced Response Levels for Bladed Discs by Mistuning:Overview of the Phenomenon[J]. Journal of Engineering for Gas Turbines & Pouver, 2011, 133(7): 1039-1051 [Article] [Google Scholar]
  16. Petrov E P. A Method for Forced Response Analysis of Mistuned Bladed Disks with Aerodynamic Effects Included[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132(6): 1-10 [Article] [Google Scholar]
  17. Petrov E P, Ewins D J. Method for Analysis of Nonlinear Multiharmonic Vibrations of Mistuned Bladed Disks with Scatter of Contact Interface Characteristics[J]. Journal of Turbomachinery, 2005, 127(1): 128-136 [Article] [CrossRef] [Google Scholar]
  18. Miyakozaw a T, Kielb R E, Hall K C, et al. The Effects of Aerodynamic Asymmetric Perturbations on Forced Response of Bladed Disks[J]. Journal of Turbomachinery, 2009, 131(10): 1-8 [Article] [Google Scholar]
  19. Kaza K R V, Kielb R E. Flutter and Response of a Mistuned Cascade in Incompressible Flow[J]. AIAA Journal, 1982, 20(20): 1120-1127 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  20. Sadeghi M, Liu F. Computation of Mistuning Effects on Cascade Flutter[J]. AIAA Journal, 2001, 39(1): 22-28 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  21. Sadeghi M, Liu F. Investigation of Mistuning Effects on Cascade Flutter Using a Coupled Method[J]. Journal of Propulsion and Power, 2007, 23(2): 266-272 [Article] [CrossRef] [Google Scholar]
  22. Quan Jinlou, Zhang Weiwei, Su Dan, et al. Flutter Analysis of Turbomachinery Cascades Based on Coupled CFD/CSD Method[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(9): 2019-2028 (in Chinese) [Article] [Google Scholar]
  23. Hanamura Y, Tanaka H, Yamaguchi K. A Simplified Method to Measure Unsteady Forces Acting on the Vibrating Blades in Cascade[J]. JSME International Journal, 2008, 23(180): 880-887 [Article] [CrossRef] [Google Scholar]
  24. Zhang Chen'an, Zhang Weiwei, Ye Zhengyin, et al. An Efficient Method on Aerodynamic Damping Coefficient Calculation for Turbomachinery[J]. Chinese Journal of Theoretical and Applied Mechanics, 2011, 43(5): 826-833 (in Chinese) [Article] [Google Scholar]
  25. Su Dan, Zhang Weiwei, Zhang Chen'an, et al. An Unsteady Aerodynamic Modeling for Turbomachinery Based on System Identification[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(2): 242-248 (in Chinese) [Article] [Google Scholar]
  26. Su Dan, Zhang Weiwei, Ye Zhengyin. A Reduced Order Model for Uncoupled and Coupled Cascade Flutter Analysis[J]. Journal of Fluids and Structures, 2016, 61: 410-430 [Article] [NASA ADS] [CrossRef] [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.