发明名称 Method and interface elements for finite-element fracture analysis
摘要 A finite element method for predicting crack opening and propagation entails defining a succession of overlapping interface elements at a potential crack plane, each element having a bound node pair and side node pairs spaced from the bound node pair to sense approach of a crack. An energy-based fracture mechanics criterion determines whether release occurs at the bound nodes and, if so, the displacement between the bound nodes is calculated based on a strain softening law. The process is repeated for each element in sequence.
申请公布号 US7505885(B2) 申请公布日期 2009.03.17
申请号 US20030350545 申请日期 2003.01.24
申请人 THE BOEING COMPANY 发明人 DEOBALD LYLE R.;DOPKER BERNHARD;MABSON GERALD E.
分类号 G06F9/455;G06F17/50 主分类号 G06F9/455
代理机构 代理人
主权项
地址