Aircraft wing design at low speeds using Taguchi method

SOYLAK M., Gokce N. K., TOPAL E. S.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, sa.1, ss.51-55, 2018 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 90 Sayı: 1
  • Basım Tarihi: 2018
  • Doi Numarası: 10.1108/aeat-06-2015-0159
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.51-55
  • Anahtar Kelimeler: Design of experiment, Taguchi method, Orthogonal indices, Reynolds number, Wing design, OPTIMIZATION, PARAMETERS, PERFORMANCE
  • Akdeniz Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of this paper is to determine the impact level of parameters affecting wing design at low speeds using Taguchi method.