Using the dynamic mesh method for genetically obtained wing structures

Vatandaş E., Özkol İ., Kaya M. O.

Aircraft Engineering and Aerospace Technology, cilt.76, sa.3, ss.314-319, 2004 (Scopus) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 76 Sayı: 3
  • Basım Tarihi: 2004
  • Doi Numarası: 10.1108/00022660410536050
  • Dergi Adı: Aircraft Engineering and Aerospace Technology
  • Derginin Tarandığı İndeksler: Scopus
  • Sayfa Sayıları: ss.314-319
  • Anahtar Kelimeler: programming and algorithm theory, flight dynamics, meshes, optimization techniques
  • İstanbul Gelişim Üniversitesi Adresli: Hayır

Özet

In this study, dynamic mesh method is implemented on a real coded genetic algorithm to demonstrate gain in computational time as well as in higher performance for optimized parameters. Since the differences developed at each step in geometries of new members are not significant, therefore, it is possible to use dynamic mesh methods for new members. In this work, because the population members are obtained by modifying the pervious ones, each member is considered as one step of geometry-change of a deforming body, for examples, a wing inflating, deflating or cambering.