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Assessment of CFD capability for hypersonic shock wave laminar boundary layer interactions using perfect gas Navier-Stokes equations
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Rouhi Youssefi, Mehrnaz. Assessment of CFD capability for hypersonic shock wave laminar boundary layer interactions using perfect gas Navier-Stokes equations. Retrieved from https://doi.org/doi:10.7282/T36D5W2N

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TitleAssessment of CFD capability for hypersonic shock wave laminar boundary layer interactions using perfect gas Navier-Stokes equations
NameRouhi Youssefi, Mehrnaz (author); Knight, Doyle (chair); Bagchi, Prosenjit (internal member); Shojaei-Zadeh, Shahab (internal member); Yan, Hong (outside member); Rutgers University; Graduate School - New Brunswick
Date Created2016
Other Date2016-01 (degree)
SubjectMechanical and Aerospace Engineering, Navier-Stokes equations, Boundary layer
Extent1 online resource (vi, 41 p. : ill.)
DescriptionThe goal of this study is to assess CFD capability for prediction of laminar shock wave/ boundary layer interactions at hypersonic velocities. More speci cally, the ow eld over a double cone con guration is simulated using perfect gas assumptions and Navier- Stokes equations. Computations are compared with experimental data obtained from measurements conducted in the LENS XX shock tunnel at CUBRC. Four separate cases of freestream conditions are simulated to examine the numerical methods in a wide range of enthalpies. The results of this investigation can provide factors for design optimization of hypersonic air vehicles. ii
NotePh.D.
NoteIncludes bibliographical references
Noteby Mehrnaz Rouhi Youssefi
Genretheses, ETD doctoral
Persistent URLhttps://doi.org/doi:10.7282/T36D5W2N
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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