Bibliographic Details
| 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] |
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| Database: |
Engineering Source |
