A novel limit distribution for the analysis of randomly mistuned bladed disks

Journal of Engineering for Gas Turbines and Power

Volumn 123, Issue 2, 2001, Pages 388-394

  Mignolet, M P ^a   Lin, C C ^a   LaBorde, B H ^a  

^a Arizona State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DISKS (MACHINE COMPONENTS); PERTURBATION TECHNIQUES; PROBABILITY DENSITY FUNCTION; RELIABILITY; RESONANCE; TUNING;

MISTUNING;

TURBOMACHINE BLADES;

MATHEMATICAL ANALYSIS;

EID: 0035302950     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1339001     Document Type: Article

References (17)

1. Effect of mistuning on the vibration of turbomachines blades induced by wakes
2. The effects of detuning upon the forced vibrations of bladed disks
3. Vibration of some structures with periodic random parameters
4. Model development and statistical investigation of turbine blade mistuning
5. Effects of structural coupling on mistuned cascade flutter and response
6. Vibration and flutter of mistuned bladed-disk assembles
7. The effects of limiting aerodynamic and structural coupling in models of mistuned bladed disk vibration
8. Calculating the statistics of forced response of a mistuned bladed disk assembly
9. Localization phenomena in mistuned assemblies with cyclic symmetry, Part I. Free vibrations
10. Localization phenomena in mistuned assemblies with cyclic symmetry. Part II. Forced vibrations
11. A higher order technique to compute the statistics of forced response of a mistuned bladed disk
12. The combined closed form-perturbation approach to the analysis of mistuned bladed disks
13. An adaptive perturbation scheme for the analysis of mistuned bladed disks
14. Direct prediction of the effects of mistuning on the forced response of bladed disks
15. On the forced response of harmonically and partially mistuned bladed disks. II. Partial mistuning and applications