Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/183654
Title: Computational Investigation of the Effect of Nose mounted Devices on the Aerothermodynamics of a Missile Shaped Body Flying at Hypersonic Speeds
Researcher: Yadav, Rajesh
Guide(s): Guven, Ugur
Keywords: Aerospace engineering
University: University of Petroleum and Energy Studies (UPES)
Completed Date: 2013
Abstract: newline
Pagination: 304p.
URI: http://hdl.handle.net/10603/183654
Appears in Departments:Department of Aerospace Engineering

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01_title.pdfAttached File27.87 kBAdobe PDFView/Open
02_certificate.pdf16.95 kBAdobe PDFView/Open
03_summary.pdf30.27 kBAdobe PDFView/Open
04_declaration.pdf10.82 kBAdobe PDFView/Open
05_acknowledgement.pdf8.25 kBAdobe PDFView/Open
06_content.pdf24.69 kBAdobe PDFView/Open
07_nomenclature.pdf31.28 kBAdobe PDFView/Open
08_list of figures.pdf51.69 kBAdobe PDFView/Open
09_list of tables.pdf4.62 kBAdobe PDFView/Open
10_chapter1.pdf455.12 kBAdobe PDFView/Open
11_chapter2.pdf192.21 kBAdobe PDFView/Open
12_chapter3.pdf1.1 MBAdobe PDFView/Open
13_chapter4.pdf1.4 MBAdobe PDFView/Open
14_chapter5.pdf8.27 MBAdobe PDFView/Open
15_chapter6.pdf4.86 MBAdobe PDFView/Open
16_chapter7.pdf48.61 kBAdobe PDFView/Open
17_reference.pdf67.22 kBAdobe PDFView/Open
18_appendix.pdf231.15 kBAdobe PDFView/Open
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