1. Shodhganga@INFLIBNET
  2. Hindustan Institute of Technology and Science
  3. Department of Aeronautical Engineering
Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/208393
Title: Effect of active and passive techniques on wing tip vortex
Researcher: Samal, Sangram Keshari
Guide(s): Shah, Dilip A
Keywords: Aerofoil
Engineering and Technology
Helmholtzs laws
Wing tip vortex
University: Hindustan University
Completed Date: 2017
Abstract: available
Pagination: 184 p.
URI: http://hdl.handle.net/10603/208393
Appears in Departments:Department of Aeronautical Engineering

Files in This Item:
File Description SizeFormat 
01_title.pdfAttached File174.91 kBAdobe PDFView/Open
02_certificate.pdf442.32 kBAdobe PDFView/Open
03_declaration.pdf241.14 kBAdobe PDFView/Open
04_abstract.pdf101.24 kBAdobe PDFView/Open
05_dedication.pdf94.95 kBAdobe PDFView/Open
06_acknowledgement.pdf96.41 kBAdobe PDFView/Open
07_table of contents.pdf196.65 kBAdobe PDFView/Open
08_list of tables.pdf179.72 kBAdobe PDFView/Open
09_list of figures.pdf356.2 kBAdobe PDFView/Open
10_abbreviations.pdf284.13 kBAdobe PDFView/Open
11_chapter 1.pdf292.91 kBAdobe PDFView/Open
12_chapter 2.pdf989.34 kBAdobe PDFView/Open
13_chapter 3.pdf104.58 kBAdobe PDFView/Open
14_chapter 4.pdf457.91 kBAdobe PDFView/Open
15_chapter 5.pdf2.66 MBAdobe PDFView/Open
16_chapter 6.pdf206.5 kBAdobe PDFView/Open
17_references.pdf270.46 kBAdobe PDFView/Open
18_appendix.pdf353.67 kBAdobe PDFView/Open
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