H2 injection and combustion in a Mach 5 air inlet through a Viscous Mach Interaction

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Title: H2 injection and combustion in a Mach 5 air inlet through a Viscous Mach Interaction
Authors: Burtschell, Yves1, Tchuen, Ghislain2 tchuengse@yahoo.com, Zeitoun, David E.1
Source: European Journal of Mechanics B: Fluids. Sep2010, Vol. 29 Issue 5, p351-356. 6p.
Subjects: Viscous flow, Hydrogen, Combustion, Mach's principle, Numerical analysis, Mechanical shock, Boundary layer (Aerodynamics), Hypersonic aerodynamics
Abstract: Abstract: Hydrogen injection has been investigated numerically in a flow configuration caused by strong shock–boundary layer interaction named Viscous Mach Interaction (VMI). The geometry that leads to this configuration is used as a hypersonic inlet. The subsonic zone, because of boundary layer detachment, allows hydrogen to be injected along the wall of the central body where combustion processes occur along a slip line when hydrogen is mixed with the incoming air flow far from the wall of the central body. [Copyright &y& Elsevier]
Copyright of European Journal of Mechanics B: Fluids is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
Database: Engineering Source
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DbLabel: Engineering Source
An: 51844245
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PubTypeId: academicJournal
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  Data: <searchLink fieldCode="DE" term="%22Viscous+flow%22">Viscous flow</searchLink><br /><searchLink fieldCode="DE" term="%22Hydrogen%22">Hydrogen</searchLink><br /><searchLink fieldCode="DE" term="%22Combustion%22">Combustion</searchLink><br /><searchLink fieldCode="DE" term="%22Mach's+principle%22">Mach's principle</searchLink><br /><searchLink fieldCode="DE" term="%22Numerical+analysis%22">Numerical analysis</searchLink><br /><searchLink fieldCode="DE" term="%22Mechanical+shock%22">Mechanical shock</searchLink><br /><searchLink fieldCode="DE" term="%22Boundary+layer+%28Aerodynamics%29%22">Boundary layer (Aerodynamics)</searchLink><br /><searchLink fieldCode="DE" term="%22Hypersonic+aerodynamics%22">Hypersonic aerodynamics</searchLink>
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  Data: Abstract: Hydrogen injection has been investigated numerically in a flow configuration caused by strong shock–boundary layer interaction named Viscous Mach Interaction (VMI). The geometry that leads to this configuration is used as a hypersonic inlet. The subsonic zone, because of boundary layer detachment, allows hydrogen to be injected along the wall of the central body where combustion processes occur along a slip line when hydrogen is mixed with the incoming air flow far from the wall of the central body. [Copyright &y& Elsevier]
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  Data: <i>Copyright of European Journal of Mechanics B: Fluids is the property of Elsevier B.V. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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RecordInfo BibRecord:
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      – Type: doi
        Value: 10.1016/j.euromechflu.2010.03.007
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      – Code: eng
        Text: English
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        PageCount: 6
        StartPage: 351
    Subjects:
      – SubjectFull: Viscous flow
        Type: general
      – SubjectFull: Hydrogen
        Type: general
      – SubjectFull: Combustion
        Type: general
      – SubjectFull: Mach's principle
        Type: general
      – SubjectFull: Numerical analysis
        Type: general
      – SubjectFull: Mechanical shock
        Type: general
      – SubjectFull: Boundary layer (Aerodynamics)
        Type: general
      – SubjectFull: Hypersonic aerodynamics
        Type: general
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      – TitleFull: H2 injection and combustion in a Mach 5 air inlet through a Viscous Mach Interaction
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            NameFull: Tchuen, Ghislain
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            NameFull: Zeitoun, David E.
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            – D: 01
              M: 09
              Text: Sep2010
              Type: published
              Y: 2010
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              Value: 29
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