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Numerical investigation of energy deposition for supersonic flow over a 2-D diamond-shaped airfoil
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Zhu, Ye. Numerical investigation of energy deposition for supersonic flow over a 2-D diamond-shaped airfoil. Retrieved from https://doi.org/doi:10.7282/T32F7N5Z

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TitleNumerical investigation of energy deposition for supersonic flow over a 2-D diamond-shaped airfoil
NameZhu, Ye (author); Knight, Doyle D (chair); Shan, Jerry (internal member); Rossmann, Tobias (internal member); Rutgers University; Graduate School - New Brunswick
Date Created2010
Other Date2010-10 (degree)
SubjectMechanical and Aerospace Engineering, Aerofoils, Air flow, Inviscid flow
Extentxv, 129 p. : ill.
DescriptionThe research models inviscid compressible flow at Mach 2 over a two dimensional diamond-shaped airfoil. The objective is to study the interaction of the energy deposition added in the upstream flow on the airfoil. Theoretical results without energy deposition in the inlet boundary and numerical results with no filaments, infinitely long symmetric filament, symmetric pulsed filament, and asymmetric pulsed filament, for Mach number, temperature, pressure in the flow field domain, are obtained. An analysis is performed on the drag coefficient acting on the airfoil. FLUENT, Gambit, and C++ are used for the numerical simulation.
NoteM.S.
NoteIncludes bibliographical references
Noteby Ye Zhu
Genretheses, ETD graduate
Persistent URLhttps://doi.org/doi:10.7282/T32F7N5Z
Languageeng
CollectionGraduate School - New Brunswick Electronic Theses and Dissertations
Organization NameRutgers, The State University of New Jersey
RightsThe author owns the copyright to this work.
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