Abstract
The vibration and stability problems of an orthotropic rectangular plate subjected to a combination of a non-conservative follower force and conservative normal force are studied. Following Brunelle and Oyibo, we investigate the dynamic behavior of an orthotropic plate in the affine space. The finite element method is used to obtain the flutter frequencies and flutter loads of orthotropic plates. The effect of elastic foundation is also considered. The material constant D* is found to have significant effect on the flutter load.
| Original language | English |
|---|---|
| Title of host publication | American Society of Mechanical Engineers, Design Engineering Division (Publication) DE |
| Editors | T.C. Huang, A.V. Karvelis |
| Publisher | ASME |
| Pages | 5-10 |
| Number of pages | 6 |
| Volume | 8 |
| Publication status | Published - 1987 |
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All Science Journal Classification (ASJC) codes
- Engineering(all)
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VIBRATIONS OF AN ORTHOTROPIC PLATE SUBJECTED TO A FOLLOWER FORCE. / Chen, Lien-Wen; Yu, C. Y.
American Society of Mechanical Engineers, Design Engineering Division (Publication) DE. ed. / T.C. Huang; A.V. Karvelis. Vol. 8 ASME, 1987. p. 5-10.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - VIBRATIONS OF AN ORTHOTROPIC PLATE SUBJECTED TO A FOLLOWER FORCE.
AU - Chen, Lien-Wen
AU - Yu, C. Y.
PY - 1987
Y1 - 1987
N2 - The vibration and stability problems of an orthotropic rectangular plate subjected to a combination of a non-conservative follower force and conservative normal force are studied. Following Brunelle and Oyibo, we investigate the dynamic behavior of an orthotropic plate in the affine space. The finite element method is used to obtain the flutter frequencies and flutter loads of orthotropic plates. The effect of elastic foundation is also considered. The material constant D* is found to have significant effect on the flutter load.
AB - The vibration and stability problems of an orthotropic rectangular plate subjected to a combination of a non-conservative follower force and conservative normal force are studied. Following Brunelle and Oyibo, we investigate the dynamic behavior of an orthotropic plate in the affine space. The finite element method is used to obtain the flutter frequencies and flutter loads of orthotropic plates. The effect of elastic foundation is also considered. The material constant D* is found to have significant effect on the flutter load.
UR - http://www.scopus.com/inward/record.url?scp=0023577961&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0023577961&partnerID=8YFLogxK
M3 - Conference contribution
VL - 8
SP - 5
EP - 10
BT - American Society of Mechanical Engineers, Design Engineering Division (Publication) DE
A2 - Huang, T.C.
A2 - Karvelis, A.V.
PB - ASME
ER -