Flexural-Torsional Flutter and Buckling of Braced Foil Beams under a Follower Force
Joint Authors
D’Annibale, Francesco
Ferretti, M.
Luongo, Angelo
Source
Mathematical Problems in Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-10, 10 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-10-12
Country of Publication
Egypt
No. of Pages
10
Main Subjects
Abstract EN
The flutter and buckling behavior of a cantilever foil beam, loaded at the tip by a follower force, are addressed in this paper.
The beam is internally and externally damped and braced at the tip by a linear spring-damper device, which is located in an eccentric position with respect to beam axis, thus coupling the flexural and torsional behaviors.
An exact linear stability analysis is carried out, and the linear stability diagram of the trivial rectilinear configuration is built up in the space of the follower load and spring’s stiffness parameters.
The effects of the flexural-torsional coupling, as well as of the damping, on the flutter and buckling critical loads are discussed.
American Psychological Association (APA)
Ferretti, M.& D’Annibale, Francesco& Luongo, Angelo. 2017. Flexural-Torsional Flutter and Buckling of Braced Foil Beams under a Follower Force. Mathematical Problems in Engineering،Vol. 2017, no. 2017, pp.1-10.
https://search.emarefa.net/detail/BIM-1189910
Modern Language Association (MLA)
Ferretti, M.…[et al.]. Flexural-Torsional Flutter and Buckling of Braced Foil Beams under a Follower Force. Mathematical Problems in Engineering No. 2017 (2017), pp.1-10.
https://search.emarefa.net/detail/BIM-1189910
American Medical Association (AMA)
Ferretti, M.& D’Annibale, Francesco& Luongo, Angelo. Flexural-Torsional Flutter and Buckling of Braced Foil Beams under a Follower Force. Mathematical Problems in Engineering. 2017. Vol. 2017, no. 2017, pp.1-10.
https://search.emarefa.net/detail/BIM-1189910
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1189910