Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/519912
Title: Experimental investigation of the effect of tabbed chevron on mixing characteristics of high speed co flow jets
Researcher: Saravanan A R
Guide(s): Thanigaiarasu S
Keywords: co-flow baseline
Engineering
Engineering and Technology
Engineering Mechanical
primary nozzle
radial Mach decay
University: Anna University
Completed Date: 2023
Abstract: newlineThe results of centerline Mach decay plots at Mach 0.6 show the tabbed chevron with two tabs as effective in reducing the potential core length by 88.3% whereas, it was 67% for tabbed chevron with eight tabs, and for chevron nozzle it was 24% when compared to the baseline nozzle configuration. At Mach 0.8, it was 85.69% for tabbed chevron with two tabs, 61% for tabbed chevron with eight tabs, and 8% for chevron nozzles respectively. The potential core length reduction of tabbed chevron (two tabs) was 76.92%, tabbed chevron with eight tabs was 49.85% and chevron nozzle was 15% for Mach 1.0 jet. The maximum decay rate is given by tabbed chevron (2 tabs) when compared to the other three geometries, showing improvement in the jet mixing as a result of the combined effect of chevron with tabs (tabbed chevron) due to stream wise vortices generated by chevrons and transverse vortices shed by tabs which is transformed into axial vortices along the downstream directions.
Pagination: xvi, 157.p
URI: http://hdl.handle.net/10603/519912
Appears in Departments:Faculty of Mechanical Engineering

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01_title.pdfAttached File20.88 kBAdobe PDFView/Open
02_prelim_pages.pdf1.18 MBAdobe PDFView/Open
03_content.pdf90.98 kBAdobe PDFView/Open
04_abstract.pdf85.11 kBAdobe PDFView/Open
05_chapter 1.pdf708.04 kBAdobe PDFView/Open
06_chapter 2.pdf114.88 kBAdobe PDFView/Open
07_chapter 3.pdf606.05 kBAdobe PDFView/Open
08_chapter 4.pdf2.04 MBAdobe PDFView/Open
09_chapter 5.pdf43.6 kBAdobe PDFView/Open
10_annexures.pdf107.85 kBAdobe PDFView/Open
80_recommendation.pdf67.3 kBAdobe PDFView/Open
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