Influence of tab corner geometry on supersonic jets

Quadros J. D., Khan S. A., Hanumantharaya R.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.93, sa.10, ss.1656-1663, 2021 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 93 Sayı: 10
  • Basım Tarihi: 2021
  • Doi Numarası: 10.1108/aeat-03-2021-0092
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
  • Sayfa Sayıları: ss.1656-1663
  • Anahtar Kelimeler: Nozzle, Core length (CL), Nozzle pressure ratio (NPR), Tab, Uncontrolled jet, Waves
  • İstanbul Teknik Üniversitesi Adresli: Evet

Özet

Purpose The purpose of this study is to evaluate the effect of tabs having different corner geometries on the flow characteristics of a supersonic convergent-divergent (C-D) nozzle.