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Title: Aerodynamic Analysis of Supersonic Biplane using Computational Fluid Dynamics
Researcher: Patidar, Vijay Kumar
Guide(s): Yadav, Rajesh, Guven, Ugur
Keywords: Engineering and Technology,Engineering,Engineering Aerospace,Supersonic Aircraft
University: University of Petroleum and Energy Studies (UPES)
Completed Date: 7/1/2017
Abstract: Staggered configurations have been proposed for the performance enhancement of these biplanes at off-design conditions. The staggered biplanes are designed in such a way that the throat area of the Busemann biplane increases and reduces the flow chocking characteristics. The lift and drag coefficients of various staggered configurations wherein the lower element of the Busemann biplane is shifted backwards by a distance of 0.1c, 0.2c, 0.3c, 0.4c and 0.5c from its original position is studied. In supersonic flow, the shock waves are generated at the sharp edge, hence the pressure at the sharp edge becomes very large and generate large amount of force at the sharp edge. The edge of the element must be strong enough to resist the pressure increment by the shock waves; therefore it is necessary to use the rounded leading edge. Keeping this aspect in view, staggered Busemann biplanes with different leading edge and trailing edge radii has also been studied using Computational Fluid Dynamics. newline
Appears in Departments:Department of Aerospace Engineering

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01_title.pdfAttached File34.84 kBAdobe PDFView/Open
02_certificate.pdf90.16 kBAdobe PDFView/Open
03_declaration.pdf80.01 kBAdobe PDFView/Open
04_acknowledgement.pdf30.3 kBAdobe PDFView/Open
05_abstracts.pdf320.84 kBAdobe PDFView/Open
06_contents.pdf134.27 kBAdobe PDFView/Open
07_list of figures.pdf420.72 kBAdobe PDFView/Open
08_list of tables.pdf20.12 kBAdobe PDFView/Open
09_nomenclature.pdf233.55 kBAdobe PDFView/Open
10_list of abbreviations.pdf27.97 kBAdobe PDFView/Open
11_chapter1.pdf3.34 MBAdobe PDFView/Open
12_chapter2.pdf1.18 MBAdobe PDFView/Open
13_chapter3.pdf199.51 kBAdobe PDFView/Open
14_chapter4.pdf4.03 MBAdobe PDFView/Open
15_chapter5.pdf4.99 MBAdobe PDFView/Open
16_chapter6.pdf348.24 kBAdobe PDFView/Open
17_chapter7.pdf757.51 kBAdobe PDFView/Open
18_annexures.pdf4.23 MBAdobe PDFView/Open

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