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International Journal for Research Trends and Innovation
International Peer Reviewed & Refereed Journals, Open Access Journal
ISSN Approved Journal No: 2456-3315 | Impact factor: 8.14 | ESTD Year: 2016
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Issue: April 2026
Volume 11 | Issue 4
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Impact Factor : 8.14
Issue per Year : 12
Volume Published : 11
Issue Published : 119
Article Submitted : 23355
Article Published : 9033
Total Authors : 23952
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| Paper Title: | Effect of corrugation geometry on the mixing characteristics of supersonic jet |
| Authors Name: | Tanya Kumari , J Aishwarya |
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IJRTI_208302
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| Published Paper Id: | IJRTI2604029 |
| Published In: | Volume 11 Issue 4, April-2026 |
| DOI: | |
| Abstract: | The effect of corrugation on the mixing promoting performance of a limiting tab will be assessed by studying the decay of a jet emerging from a convergent-divergent nozzle, with a limiting tab, with and without corrugation, running along a diameter at the nozzle exit, operated at certain nozzle pressure ratios. Uncontrolled jet was also will be studied for comparison. The physics behind the difference between the mixing caused by the uncorrugated and corrugated tabs in the presence of adverse and favourable pressure gradient will be addressed using the density gradient contours of the jet core as the main source and the centerline Mach number decay as the supporting material. Unsteady Reynolds averaged Navier stokes equation will be solved using Ansys CFX tool.The physics behind the difference between the mixing caused by the uncorrugated and corrugated tabs in the presence of adverse and favorable pressure gradient is addressed using the shadowgraph images of the jet core as the main source and the centerline pitot pressure decay as the supporting material. The results show that the mixing promotion caused by the tabs leads to the shortening of the third and fourth shock cells in the jet core. This can be regarded as an advantage from the screech suppression point of view. |
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| Cite Article: | "Effect of corrugation geometry on the mixing characteristics of supersonic jet ", International Journal for Research Trends and Innovation (www.ijrti.org), ISSN:2456-3315, Vol.11, Issue 4, page no.a201-a206, April-2026, Available :http://www.ijrti.org/papers/IJRTI2604029.pdf |
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2456-3315 | IMPACT FACTOR: 8.14 Calculated By Google Scholar| ESTD YEAR: 2016 An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.14 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator |
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Published Paper ID: IJRTI2604029
Registration ID:208302
Published In: Volume 11 Issue 4, April-2026
DOI (Digital Object Identifier):
Page No: a201-a206 Country: secunderabad, telangana, India Research Area: Engineering Publisher : IJ Publication Published Paper URL : https://www.ijrti.org/viewpaperforall?paper=IJRTI2604029 Published Paper PDF: https://www.ijrti.org/papers/IJRTI2604029 |
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ISSN: 2456-3315
Impact Factor: 8.14 and ISSN APPROVED,
Journal Starting Year (ESTD) : 2016
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