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Effect of heat release on the spatial stability of a supersonic reacting mixing layer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jackson, T. L. Grosch, C. E. |
| Copyright Year | 1988 |
| Description | A numerical study of the stability of compressible mixing layers in which a diffusion flame is embedded is described. The mean velocity profile has been approximated by a hyperbolic tangent profile and the limit of infinite activation energy taken, which reduces the diffusion flame to a flame sheet. The addition of combustion in the form of a flame sheet was found to have important, and complex, effects on the flow stability. |
| File Size | 512928 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890005031 |
| Archival Resource Key | ark:/13960/t1ck3975r |
| Language | English |
| Publisher Date | 1988-11-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Flow Stability Flames Numerical Analysis Stability Supersonic Combustion Diffusion Flames Reaction Kinetics Combustion Velocity Distribution Spatial Resolution Mixing Layers Fluids Compressible Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
