作者: Michael Bruyneel , Cezar Diaconu
DOI: 10.1002/9781118097298.WEOC238
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摘要: In this article, the structural composite design process is presented. It shown that it an extremely complicated task conducted nowadays with computers and numerical tools. involves several disciplines, including computer-aided (CAD), engineering (CAE), manufacturing (CAM), in iterative where optimization plays a very important role. The CAE of structures described, ways to parameterize laminates are explained. These parameterizations form basis for introduction formulations optimal design, which main topic addressed here. Several approaches have been proposed over past years, but global solution not yet available. ultimate procedure should address problem at CAD-CAE-CAM levels simultaneously, order provide light safe designs ready manufacture. Since aeronautics industry has driven innovation most concepts described here based on developments carried out large aircrafts. Keywords: CAD; CAM; CAE; FEM; optimization; stacking sequence; aircraft