Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/31537
Title: Experimental and numerical studies on the flow characteristics of slanted entry cd nozzle in supersonic streams
Researcher: Senthilkumar C
Guide(s): Elangovan S
Keywords: cd nozzle
mechanical engineering
supersonic streams
Upload Date: 23-Dec-2014
University: Anna University
Completed Date: 01/03/2009
Abstract: Flow characteristics of straight and slanted entry CD nozzle with a newlinedesign Mach number of 294 exposed to a Mach 2 free jet has been newlineinvestigated The aim of this investigation is to find whether a nozzle exposed newlineto a supersonic free jet can choke and deliver supersonic flow at its exit newlineinspite of the presence of a detached shock standing ahead of its inlet Nozzles newlinewith straight entry inlet face normal to the flow and with slanted entry with newlineslanting angles 15 30 45 and 57 were studied The free jet expansion newlinelevel was also varied to cover a range from highly overexpanded to newlinemoderately underexpanded states The experimental results of this study newlinereveals that the nozzle placed in a Mach 2 free jet can choke and deliver newlinesupersonic flow at its exit newline newline
Pagination: xviii, 152p.
URI: http://hdl.handle.net/10603/31537
Appears in Departments:Faculty of Mechanical Engineering

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01_title.pdfAttached File38.82 kBAdobe PDFView/Open
02_certificate.pdf6.03 kBAdobe PDFView/Open
03_abstract.pdf14.01 kBAdobe PDFView/Open
04_acknowledgement.pdf7.54 kBAdobe PDFView/Open
05_contents.pdf50.4 kBAdobe PDFView/Open
06_chapter 1.pdf22.7 kBAdobe PDFView/Open
07_chapter 2.pdf704.11 kBAdobe PDFView/Open
08_chapter 3.pdf613.34 kBAdobe PDFView/Open
09_chapter 4.pdf96.98 kBAdobe PDFView/Open
10_chapter 5.pdf927.72 kBAdobe PDFView/Open
11_chapter 6.pdf19.9 kBAdobe PDFView/Open
12_appendix.pdf41.71 kBAdobe PDFView/Open
13_references.pdf60.71 kBAdobe PDFView/Open
14_publications.pdf9.97 kBAdobe PDFView/Open
15_vitae.pdf5.82 kBAdobe PDFView/Open


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