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The combined closed form-perturbation approach to the analysis of mistuned bladed disks

Author
MIGNOLET, M. P; LIN, C.-C
Arizona state univ., dep. mechanical aerospace eng., Tempe AZ 85287-6106, United States
Conference name
International gas turbine and aeroengine congress and exposition (37 ; Cologne 1992-06-01)
Source

Journal of turbomachinery. 1993, Vol 115, Num 4, pp 771-780 ; ref : 29 ref

CODEN
JOTUEI
ISSN
0889-504X
Scientific domain
Mechanical engineering; Mechanics acoustics
Publisher
American Society of Mechanical Engineers, New York, NY
Publication country
United States
Document type
Conference Paper
Language
English
Keyword (fr)
Aube turbine Equation forme close Fonction densité probabilité Fonction perturbation Lame Modèle simulation Réponse dynamique Turbomachine
Keyword (en)
Turbine blade Closed form equation Probability density function Perturbation function Blade Simulation model Dynamic response Turbomachine
Keyword (es)
Paleta turbina Ecuación forma cerrada Función densidad probabilidad Función perturbación Lámina Modelo simulación Respuesta dinámica Turbomáquina
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design / 001D12F Engines and turbines / 001D12F02 Continuous cycle engines: steam and gas turbines, jet engines

Discipline
Mechanical engineering. Mechanical construction. Handling
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
3799623

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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