Reliability of Complex Structures by Large Admissible PerturbationsSource: Journal of Offshore Mechanics and Arctic Engineering:;1993:;volume( 115 ):;issue: 003::page 167DOI: 10.1115/1.2920109Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The p erturbation a pproach to r eliability (PAR) is a powerful methodology for reliability analysis and design of large structures. Its main features are: F1) PAR provides the exact global failure equation for any failure criterion for which the corresponding structural analysis can be performed by finite elements. F2) Geometry, material, and loads appear explicitly in the global failure equations and are treated as random variables. No need arises for load path selection or load pattern specification. F3) PAR introduces an invariant and consistent redundancy definition as an injective mapping restricted on the failure surface. Thus, the redundancy/reliability of the structure is expressed in terms of the redundancy/reliability of its structural components. F4) The norm of the Rosenblatt transformed reliability injection is the reliability index. F5) For each global failure equation or combination of failure equations, PAR computes the individual or joint design points without enumerating paths to failure, trial and error, or repeated finite element analyses. F6) Serviceability or ultimate global structural failure is defined by specifying a threshold value of any quantity that can be computed by finite elements: natural frequencies, dynamic normal modes, static deflections, static stresses, buckling loads, and buckling modes are implemented in PAR. Stress failure equations are used along with linearized plasticity surfaces to identify element failure. Several applications are presented to assess PAR.
keyword(s): Reliability , Failure , Stress , Equations , Finite element analysis , Redundancy (Engineering) , Design , Buckling , Deflection , Errors , Frequency , Geometry , Plasticity , Structural analysis , Event history analysis , Structural failures AND Maintainability ,
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contributor author | E. Beyko | |
contributor author | M. M. Bernitsas | |
date accessioned | 2017-05-08T23:42:13Z | |
date available | 2017-05-08T23:42:13Z | |
date copyright | August, 1993 | |
date issued | 1993 | |
identifier issn | 0892-7219 | |
identifier other | JMOEEX-28089#167_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/112463 | |
description abstract | The p erturbation a pproach to r eliability (PAR) is a powerful methodology for reliability analysis and design of large structures. Its main features are: F1) PAR provides the exact global failure equation for any failure criterion for which the corresponding structural analysis can be performed by finite elements. F2) Geometry, material, and loads appear explicitly in the global failure equations and are treated as random variables. No need arises for load path selection or load pattern specification. F3) PAR introduces an invariant and consistent redundancy definition as an injective mapping restricted on the failure surface. Thus, the redundancy/reliability of the structure is expressed in terms of the redundancy/reliability of its structural components. F4) The norm of the Rosenblatt transformed reliability injection is the reliability index. F5) For each global failure equation or combination of failure equations, PAR computes the individual or joint design points without enumerating paths to failure, trial and error, or repeated finite element analyses. F6) Serviceability or ultimate global structural failure is defined by specifying a threshold value of any quantity that can be computed by finite elements: natural frequencies, dynamic normal modes, static deflections, static stresses, buckling loads, and buckling modes are implemented in PAR. Stress failure equations are used along with linearized plasticity surfaces to identify element failure. Several applications are presented to assess PAR. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Reliability of Complex Structures by Large Admissible Perturbations | |
type | Journal Paper | |
journal volume | 115 | |
journal issue | 3 | |
journal title | Journal of Offshore Mechanics and Arctic Engineering | |
identifier doi | 10.1115/1.2920109 | |
journal fristpage | 167 | |
journal lastpage | 178 | |
identifier eissn | 1528-896X | |
keywords | Reliability | |
keywords | Failure | |
keywords | Stress | |
keywords | Equations | |
keywords | Finite element analysis | |
keywords | Redundancy (Engineering) | |
keywords | Design | |
keywords | Buckling | |
keywords | Deflection | |
keywords | Errors | |
keywords | Frequency | |
keywords | Geometry | |
keywords | Plasticity | |
keywords | Structural analysis | |
keywords | Event history analysis | |
keywords | Structural failures AND Maintainability | |
tree | Journal of Offshore Mechanics and Arctic Engineering:;1993:;volume( 115 ):;issue: 003 | |
contenttype | Fulltext |