Design procedure for laminated composites based on genetic algorithm with function approximation

Masaru Zako, Naoki Takano, Norio Takeda

Research output: Contribution to journalArticle

Abstract

In this paper, a design procedure for laminated composite structures based on GA (Genetic Algorithms) with function approximations is proposed. Design variables considered to enhance the rigidity of the laminated composite structure are the number of laminae, the fiber orientations and the stacking sequence. The fiber orientations are chosen from some prepared angles. In the proposed procedure, the rigidity of laminated composites is approximated by means of weighing coefficients and transformed elastic constants at the prepared angles. The proposed approximate function can be thought of response surfaces, because the weighing coefficients are adjusted with pairs of input and output data. The effective approximation is generated using auxiliary information about the principal stress distribution. The approximate function is used as the objective function of GA and can be evaluated without finite element analysis. As a result, the proposed procedure can reduce computational cost remarkably. In this paper, the detail of our developed design procedure and data sampling scheme are described.

Original languageEnglish
Pages (from-to)446-451
Number of pages6
JournalZairyo/Journal of the Society of Materials Science, Japan
Volume47
Issue number5
DOIs
Publication statusPublished - 1998 May
Externally publishedYes

ASJC Scopus subject areas

  • Materials Science(all)
  • Condensed Matter Physics
  • Mechanics of Materials
  • Mechanical Engineering

Fingerprint Dive into the research topics of 'Design procedure for laminated composites based on genetic algorithm with function approximation'. Together they form a unique fingerprint.

  • Cite this