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Nonlinear modal models for sonic fatigue response prediction : a comparison of methods

Author
HOLLKAMP, Joseph J1 ; GORDON, Robert W1 ; SPOTTSWOOD, S. Michael1
[1] Air Force Research Laboratory, AFRL/VASM, 2790 D. Street, Wright-Patterson AFB, OH 45433-7402, United States
Source

Journal of sound and vibration. 2005, Vol 284, Num 3-5, pp 1145-1163, 19 p ; ref : 14 ref

CODEN
JSVIAG
ISSN
0022-460X
Scientific domain
Civil engineering; Mechanical engineering; Mechanics acoustics
Publisher
Elsevier, London
Publication country
United Kingdom
Document type
Article
Language
English
Keyword (fr)
Aéronef Effet non linéaire Fatigue acoustique Modélisation Méthode domaine temps Méthode élément fini Poutre
Keyword (en)
Aircraft Non linear effect Acoustic fatigue Modeling Time domain method Finite element method Beam(mechanics)
Keyword (es)
Aeronave Efecto no lineal Fatiga acústica Modelización Método dominio tiempo Método elemento finito Viga
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40C Acoustics / 001B40C40 Structural acoustics and vibration

Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30N Fracture mechanics (crack, fatigue, damage...)

Discipline
Physics : acoustics Physics : solid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
16790638

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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