The present paper deals with parameter identification of aluminum honeycomb sandwich panels with the assumption that they can be treated as orthotropic continua. Elastic constants and modal damping ratios are considered as the identified parameters, and the basic equations of Timoshenko beam theory
โฆ LIBER โฆ
A Timoshenko beam theory with pressure corrections for layered orthotropic beams
โ Scribed by Graeme J. Kennedy; Jorn S. Hansen; Joaquim R.R.A. Martins
- Publisher
- Elsevier Science
- Year
- 2011
- Tongue
- English
- Weight
- 452 KB
- Volume
- 48
- Category
- Article
- ISSN
- 0020-7683
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
PARAMETER IDENTIFICATION FOR ALUMINUM HO
โ
T. Saito; R.D. Parbery; S. Okuno; S. Kawano
๐
Article
๐
1997
๐
Elsevier Science
๐
English
โ 259 KB
Shear correction factors in Timoshenko's
โ
F. Gruttmann; W. Wagner
๐
Article
๐
2001
๐
Springer
๐
English
โ 264 KB
Refined solution of the timoshenko probl
โ
V. I. Shvabโyuk; Ya. M. Pasternak; S. V. Rotko
๐
Article
๐
2010
๐
Springer
๐
English
โ 342 KB
Exponential Decay Rate for a Timoshenko
โ
G. Q. Xu; S. P. Yung
๐
Article
๐
2004
๐
Springer
๐
English
โ 168 KB
Derivation of the exact stiffness matrix
โ
Quang-Huy Nguyen; Enzo Martinelli; Mohammed Hjiaj
๐
Article
๐
2011
๐
Elsevier Science
๐
English
โ 806 KB
A Mindlin plate triangular element with
โ
Soh, A. K. ;Zhifei, Long ;Song, Cen
๐
Article
๐
1999
๐
John Wiley and Sons
๐
English
โ 83 KB
๐ 2 views
A triangular plate bending element, based on the generalized conforming element theory, has been formulated. The variations of the rotation and shear strain along each side are determined based on Timoshenko's beam theory. The rotation and shear strain ยฎelds within the element are then obtained usin