A higher-order shear deformation theory is used to analyse laminated anisotropic composite plates for deflections, stresses, natural frequencies and buckling loads. The theory accounts for parabolic distribution of the transverse shear stresses, and requires no shear correction coefficients. A displ
โฆ LIBER โฆ
Free vibrations of laminated composite plates using second-order shear deformation theory
โ Scribed by A.A. Khdeir; J.N. Reddy
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 151 KB
- Volume
- 71
- Category
- Article
- ISSN
- 0045-7949
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
Analysis of laminated composite plates u
โ
N. D. Phan; J. N. Reddy
๐
Article
๐
1985
๐
John Wiley and Sons
๐
English
โ 852 KB
Finite strip analysis of anisotropic lam
โ
G. Akhras; M.S. Cheung; W. Li
๐
Article
๐
1994
๐
Elsevier Science
๐
English
โ 547 KB
Random vibrations of laminated plates mo
โ
G. Cederbaum; I. Elishakoff; L. Librescu
๐
Article
๐
1989
๐
Elsevier Science
๐
English
โ 508 KB
Large Amplitude Flexural Vibration Of La
Large Amplitude Flexural Vibration Of Laminated Plates Using A Higher Order Shear Deformation Theory
โ
R. Tenneti; K. Chandrashekhara
๐
Article
๐
1994
๐
Elsevier Science
๐
English
โ 195 KB
Flexural analysis of laminated composite
โ
T.K. Paul; K.M. Rao
๐
Article
๐
1995
๐
Elsevier Science
๐
English
โ 584 KB
Vibration Analysis Of Laminated Plates U
โ
J.-F. He; B.-A. Ma
๐
Article
๐
1994
๐
Elsevier Science
๐
English
โ 373 KB
A previously published discrete-layer shear deformation theory is used to analyze free vibration of laminated plates. The theory includes the assumption that the transverse shear strains across any two layers are linearly dependent on each other. The theory has the same dependent variables as first