Manipulation of Supersonic Jet using Grooved Tabs

This study experimentally evaluated the mixing augmentation of twin tabs mounted along a diameter at the outlet of a convergent-divergent Mach 1.62 circular nozzle. The usefulness of the plain and grooved tabs is examined at various expansion levels prevailing at nozzle outlet. The tab's perfor...

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Bibliographic Details
Main Authors: A. K. Mali, T. Jana, M. Kaushik, S. Thanigaiarasu
Format: Article
Language:English
Published: Isfahan University of Technology 2024-02-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:https://www.jafmonline.net/article_2404_30ee2f8d71b708906d826879b71f4ca9.pdf

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