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A comprehensive model to determine the effects of temperature and species fluctuations on reaction rates in turbulent reaction flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Diskin, G. Matulaitis, J. Magnotti, F. Chinitz, W. |
| Copyright Year | 1984 |
| Description | The use of silane (SiH4) as an effective ignitor and flame stabilizing pilot fuel is well documented. A reliable chemical kinetic mechanism for prediction of its behavior at the conditions encountered in the combustor of a SCRAMJET engine was calculated. The effects of hydrogen addition on hydrocarbon ignition and flame stabilization as a means for reduction of lengthy ignition delays and reaction times were studied. The ranges of applicability of chemical kinetic models of hydrogen-air combustors were also investigated. The CHARNAL computer code was applied to the turbulent reaction rate modeling. |
| File Size | 4060833 |
| Page Count | 110 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840009452 |
| Archival Resource Key | ark:/13960/t7hq8sb90 |
| Language | English |
| Publisher Date | 1984-01-31 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Silanes Turbulence Additives Flame Stability Coding Supersonic Combustion Ramjet Engines Reaction Kinetics Ignition Performance Prediction Mathematical Models Computer Programs Time Lag 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 |
