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Title: Effect of rib on suddenly expanded supersonic flow
Researcher: Vijayaraja K
Guide(s): Elangovan S
Keywords: mechanical engineering
rib on suddenly
supersonic flow
Upload Date: 10-Dec-2014
University: Anna University
Completed Date: 01/04/2009
Abstract: The base pressure field and the wall pressure distribution along the newlineenlarged duct for subsonic correctly underexpanded sonic and supersonic newlineflow at different expansion have been studied experimentally For generation newlineof subsonic Mach number and correctly underexpanded sonic flows a newlineconvergent nozzle was used and for supersonic flow generation a convergent newlinedivergent nozzle of suitable area ratio was employed The flow from these newlineaxisymmetric nozzles was suddenly expanded into a straight tube of larger newlinecross section area than the nozzle exit area The ratio of enlarged duct area to newlinenozzle exit area was 484 in the present investigation For all the experimental newlineruns the flow through enlarged duct was discharged into the ambient atmosphere newline newline
Pagination: xxi, 191p.
Appears in Departments:Faculty of Mechanical Engineering

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01_title.pdfAttached File36.95 kBAdobe PDFView/Open
02_certificate.pdf5.84 kBAdobe PDFView/Open
03_abstract.pdf15.65 kBAdobe PDFView/Open
04_acknowledgement.pdf7.04 kBAdobe PDFView/Open
05_contents.pdf27.43 kBAdobe PDFView/Open
06_chapter 1.pdf27.63 kBAdobe PDFView/Open
07_chapter 2.pdf147.95 kBAdobe PDFView/Open
08_chapter 3.pdf3.87 MBAdobe PDFView/Open
09_chapter 4.pdf4.68 MBAdobe PDFView/Open
10_chapter 5.pdf23.53 kBAdobe PDFView/Open
11_appendix.pdf41.71 kBAdobe PDFView/Open
12_references.pdf39.7 kBAdobe PDFView/Open
13_publications.pdf8.2 kBAdobe PDFView/Open
14_vitae.pdf6.11 kBAdobe PDFView/Open

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