Influence of tab corner geometry on supersonic jets

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

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2021 (SCI-Expanded) identifier identifier

  • Publication Type: Article / Article
  • Volume:
  • Publication Date: 2021
  • Doi Number: 10.1108/aeat-03-2021-0092
  • Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
  • Keywords: Nozzle, Core length (CL), Nozzle pressure ratio (NPR), Tab, Uncontrolled jet, Waves
  • Istanbul Technical University Affiliated: Yes

Abstract

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.