𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Finite element analysis of 3-ply laminated conical shell for flutter

✍ Scribed by P. J. Sunder; C. V. Ramakrishnan; S. Sengupta

Publisher
John Wiley and Sons
Year
1983
Tongue
English
Weight
425 KB
Volume
19
Category
Article
ISSN
0029-5981

No coin nor oath required. For personal study only.

✦ Synopsis

The results of the finite element analysis of 3-ply laminated conical shells with light core for linear panel flutter are presented and certain advantages of such shells discussed.

πŸ“œ SIMILAR VOLUMES

FINITE ELEMENT TRANSIENT DYNAMIC ANALYSI
FINITE ELEMENT TRANSIENT DYNAMIC ANALYSIS OF LAMINATED STIFFENED SHELLS
✍ B.GANGADHARA PRUSTY; S.K. SATSANGI πŸ“‚ Article πŸ“… 2001 πŸ› Elsevier Science 🌐 English βš– 400 KB

The present work describes the transient dynamic response of unsti!ened/sti!ened composite plates/shells using "nite element method. Composite panels "nd wide applications in aerospace, marine and other engineering because of its high strength to weight ratios. These structures are often subjected t

A novel 3D mixed finite-element model fo
A novel 3D mixed finite-element model for statics of angle-ply laminates
✍ Y. M. Desai; G. S. Ramtekkar; A. H. Shah πŸ“‚ Article πŸ“… 2003 πŸ› John Wiley and Sons 🌐 English βš– 223 KB πŸ‘ 1 views

## Abstract Analysis of angle‐ply laminates becomes critical and computationally involved because of the presence of extension–shear coupling. A refined three‐dimensional, mixed, 18‐node finite element (FE) model has been developed to analyse angle‐ply laminates under static loading. The minimum po

FINITE ELEMENT FREE VIBRATION ANALYSIS O
FINITE ELEMENT FREE VIBRATION ANALYSIS OF DOUBLY CURVED LAMINATED COMPOSITE SHELLS
✍ D. Chakravorty; J.N. Bandyopadhyay; P.K. Sinha πŸ“‚ Article πŸ“… 1996 πŸ› Elsevier Science 🌐 English βš– 409 KB

A finite element analysis for the free vibration behaviour of doubly curved shells is presented in which eight-noded curved quadrilateral isoparametric finite elements are used. The first order shear deformation theory for thin and shallow shells is used in the formulation. Results are obtained for

A nine-node assumed strain finite elemen
A nine-node assumed strain finite element for large-deformation analysis of laminated shells
✍ S. J. Lee; W. Kanok-Nukulchai πŸ“‚ Article πŸ“… 1998 πŸ› John Wiley and Sons 🌐 English βš– 252 KB πŸ‘ 2 views

An application of the element-based Lagrangian formulation is described for large-deformation analysis of both single-layered and laminated shells. Natural co-ordinate-based stresses, strains and constitutive equations are used throughout the formulation of the present shell element which o ers sign