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Shock wave laminar boundary layer interaction over a double wedge in a high mach number flow
Descriptive
TitleInfo
Title
Shock wave laminar boundary layer interaction over a double wedge in a high mach number flow
Name
(type = personal)
NamePart
(type = family)
Badr
NamePart
(type = given)
Mohammad Ali
DisplayForm
Mohammad Ali Badr
Role
RoleTerm
(authority = RULIB)
author
Name
(type = personal)
NamePart
(type = family)
Knight
NamePart
(type = given)
Dyole D.
DisplayForm
Dyole D. Knight
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
chair
Name
(type = personal)
NamePart
(type = family)
Jaluria
NamePart
(type = given)
Yogesh
DisplayForm
Yogesh Jaluria
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
internal member
Name
(type = personal)
NamePart
(type = family)
Diez-Garias
NamePart
(type = given)
F. Javier
DisplayForm
F. Javier Diez-Garias
Affiliation
Advisory Committee
Role
RoleTerm
(authority = RULIB)
internal member
Name
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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)
Shock wave laminar boundary layer interaction (SWBLI) over a double wedge was simulated at Mach 7.11 with stagnation enthalpy of 2 MJ/kg (low enthalpy case), and at Mach 7.14 with stagnation enthalpy of 8 MJ/kg (high enthalpy case) using the commercial flow solver GASPex. An inviscid simulation was performed at Mach 7.14 for validation and solution justification. In the inviscid case, the region downstream of the first shock wave shows less than one percent difference for any flow parameter in comparison with oblique shock wave theory. In both cases, the flow is assumed to be laminar. The computed heat transfer distribution agrees closely with the experiment at the time reported by experiment where the flow reaches steady state; however, significant difference are evident in the duration in which the flow reaches steady state in the computation. In particular, the time-accurate simulations indicate a significantly longer physical time to achieve steady state than observed in the experiment.
Subject
(authority = RUETD)
Topic
Mechanical and Aerospace Engineering
Subject
(authority = ETD-LCSH)
Topic
Shock (Mechanics)
Subject
(authority = ETD-LCSH)
Topic
Laminar flow
Subject
(authority = ETD-LCSH)
Topic
Laminar boundary layer
Subject
(authority = ETD-LCSH)
Topic
Heat--Transmission
RelatedItem
(type = host)
TitleInfo
Title
Rutgers University Electronic Theses and Dissertations
Identifier
(type = RULIB)
ETD
Identifier
ETD_6948
PhysicalDescription
Form
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electronic resource
InternetMediaType
application/pdf
InternetMediaType
text/xml
Extent
1 online resource (viii, 44 p. : ill.)
Note
(type = degree)
M.S.
Note
(type = bibliography)
Includes bibliographical references
Note
(type = special display note)
by Mohammad Ali Badr
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/T3C24ZGK
Genre
(authority = ExL-Esploro)
ETD graduate
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Rights
RightsDeclaration
(ID = rulibRdec0006)
The author owns the copyright to this work.
RightsHolder
(type = personal)
Name
FamilyName
Badr
GivenName
Mohammad
MiddleName
Ali
Role
Copyright Holder
RightsEvent
Type
Permission or license
DateTime
(encoding = w3cdtf);
(qualifier = exact);
(point = start)
2015-12-22 17:10:13
AssociatedEntity
Name
Mohammad Badr
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.
Copyright
Status
Copyright protected
Availability
Status
Open
Reason
Permission or license
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Technical
RULTechMD
(ID = TECHNICAL1)
ContentModel
ETD
OperatingSystem
(VERSION = 5.1)
windows xp
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