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