RUcore: Rutgers University Community Repository
Assessment of CFD capability for hypersonic shock wave laminar boundary layer interactions using perfect gas Navier-Stokes equations
Descriptive
TitleInfo
Title
Assessment of CFD capability for hypersonic shock wave laminar boundary layer interactions using perfect gas Navier-Stokes equations
Name
(type = personal)
NamePart
(type = family)
Rouhi Youssefi
NamePart
(type = given)
Mehrnaz
NamePart
(type = date)
1985-
DisplayForm
Mehrnaz Rouhi Youssefi
Role
RoleTerm
(authority = RULIB)
author
Name
(type = personal)
NamePart
(type = family)
Knight
NamePart
(type = given)
Doyle
DisplayForm
Doyle Knight
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
chair
Name
(type = personal)
NamePart
(type = family)
Bagchi
NamePart
(type = given)
Prosenjit
DisplayForm
Prosenjit Bagchi
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
internal member
Name
(type = personal)
NamePart
(type = family)
Shojaei-Zadeh
NamePart
(type = given)
Shahab
DisplayForm
Shahab Shojaei-Zadeh
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
internal member
Name
(type = personal)
NamePart
(type = family)
Yan
NamePart
(type = given)
Hong
DisplayForm
Hong Yan
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
outside member
Name
(type = corporate)
NamePart
Rutgers University
Role
RoleTerm
(authority = RULIB)
degree grantor
Name
(type = corporate)
NamePart
Graduate School - New Brunswick
Role
RoleTerm
(authority = RULIB)
school
TypeOfResource
Text
Genre
(authority = marcgt)
theses
OriginInfo
DateCreated
(encoding = w3cdtf);
(qualifier = exact)
2016
DateOther
(qualifier = exact);
(type = degree)
2016-01
CopyrightDate
(encoding = w3cdtf);
(qualifier = exact)
2016
Place
PlaceTerm
(type = code)
xx
Language
LanguageTerm
(authority = ISO639-2b);
(type = code)
eng
Abstract
(type = abstract)
The 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
Subject
(authority = RUETD)
Topic
Mechanical and Aerospace Engineering
RelatedItem
(type = host)
TitleInfo
Title
Rutgers University Electronic Theses and Dissertations
Identifier
(type = RULIB)
ETD
Identifier
ETD_7027
PhysicalDescription
Form
(authority = gmd)
electronic resource
InternetMediaType
application/pdf
InternetMediaType
text/xml
Extent
1 online resource (vi, 41 p. : ill.)
Note
(type = degree)
Ph.D.
Note
(type = bibliography)
Includes bibliographical references
Subject
(authority = ETD-LCSH)
Topic
Navier-Stokes equations
Subject
(authority = ETD-LCSH)
Topic
Boundary layer
Note
(type = statement of responsibility)
by Mehrnaz Rouhi Youssefi
RelatedItem
(type = host)
TitleInfo
Title
Graduate School - New Brunswick Electronic Theses and Dissertations
Identifier
(type = local)
rucore19991600001
Location
PhysicalLocation
(authority = marcorg);
(displayLabel = Rutgers, The State University of New Jersey)
NjNbRU
Identifier
(type = doi)
doi:10.7282/T36D5W2N
Genre
(authority = ExL-Esploro)
ETD doctoral
Back to the top
Rights
RightsDeclaration
(ID = rulibRdec0006)
The author owns the copyright to this work.
RightsHolder
(type = personal)
Name
FamilyName
Rouhi Youssefi
GivenName
Mehrnaz
Role
Copyright Holder
RightsEvent
Type
Permission or license
DateTime
(encoding = w3cdtf);
(qualifier = exact);
(point = start)
2016-01-19 12:40:53
AssociatedEntity
Name
Mehrnaz Rouhi Youssefi
Role
Copyright holder
Affiliation
Rutgers University. Graduate School - New Brunswick
AssociatedObject
Type
License
Name
Author Agreement License
Detail
I hereby grant to the Rutgers University Libraries and to my school the non-exclusive right to archive, reproduce and distribute my thesis or dissertation, in whole or in part, and/or my abstract, in whole or in part, in and from an electronic format, subject to the release date subsequently stipulated in this submittal form and approved by my school. I represent and stipulate that the thesis or dissertation and its abstract are my original work, that they do not infringe or violate any rights of others, and that I make these grants as the sole owner of the rights to my thesis or dissertation and its abstract. I represent that I have obtained written permissions, when necessary, from the owner(s) of each third party copyrighted matter to be included in my thesis or dissertation and will supply copies of such upon request by my school. I acknowledge that RU ETD and my school will not distribute my thesis or dissertation or its abstract if, in their reasonable judgment, they believe all such rights have not been secured. I acknowledge that I retain ownership rights to the copyright of my work. I also retain the right to use all or part of this thesis or dissertation in future works, such as articles or books.
RightsEvent
DateTime
(encoding = w3cdtf);
(qualifier = exact);
(point = start)
2016-01-31
DateTime
(encoding = w3cdtf);
(qualifier = exact);
(point = end)
2017-01-30
Type
Embargo
Detail
Access to this PDF has been restricted at the author's request. It will be publicly available after January 30th, 2017.
Copyright
Status
Copyright protected
Availability
Status
Open
Reason
Permission or license
Back to the top
Technical
RULTechMD
(ID = TECHNICAL1)
ContentModel
ETD
OperatingSystem
(VERSION = 5.1)
windows xp
Back to the top
Statistical Profile