Published 1982 | Version v1
Miscellaneous

Limits of collapse load for axyssimmetricals shells and plates

  • 1. Piaui Univ., Teresina (Brazil). Dept. de Estruturas
  • 2. Rio de Janeiro Univ. (Brazil). Coordenacao dos Programas de Pos-graduacao de Engenharia

Description

The rigid-plastic limit analysis of shells of revolution and circular plates submmited to loads rotationally symetric is studied. The finite element method is used. The von Mises criteria that is used in sandwich shells is adopted. This criteria reduces the limit analysis problem in the application of the nonlinear programming techniques. Some results on the lower and upper limits of the collapse load are presented. (E.G.)

Abstract (Portuguese)

Estuda-se a analise limite rigido-plastica de cascas de revolucao e placas circulares sujeitas a carregamento rotacionalmente simetrico. Discretiza-se a estrutura atraves do MEF. Adota-se o criterio de von Mises valido para 'casca sandwich', o que reduz o problema de analise limite na aplicacao de tecnicas de programacao nao-linear. Apresentam-se resultados de limites superiores e inferiores da carga de colapso. (E.G.)

Additional details

Additional titles

Original title (Portuguese)
Limites da carga de colapso de cascas e placas axissimetricas

Publishing Information

Imprint Title
Proceedings of the 2. Brazilian Symposium on Pipes and Pressure Vessels. V. 1, 2
Imprint Pagination
643 p.
Journal Page Range
p. 561-579.
Report number
INIS-BR--173

Conference

Title
2. Brazilian Symposium on Pipes and Pressure Vessels.
Dates
24-26 Nov 1982.
Place
Salvador, BA (Brazil).

INIS

Country of Publication
Brazil
Country of Input or Organization
Brazil
INIS RN
15067937
Subject category
S22: GENERAL STUDIES OF NUCLEAR REACTORS;
Resource subtype / Literary indicator
Conference
Descriptors DEI
FINITE ELEMENT METHOD; PLASTICITY; SHELLS; STATIC LOADS
Descriptors DEC
MECHANICAL PROPERTIES; NUMERICAL SOLUTION

Optional Information

Notes
Imprint:Anais do 2. Simposio Brasileiro sobre Tubulacoes e Vasos de Pressao. V. 1, 2.