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Investigation of critical burning of fuel droplets. [monopropellants
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chanin, S. Faeth, G. M. |
| Copyright Year | 1974 |
| Description | The steady combustion characteristics of droplets were considered in combustion chamber environments at various pressures, flow conditions, and ambient oxidizer concentrations for a number of hydrocarbon fuels. Using data obtained earlier, predicted gasification rates were within + or - 30% of measurements when the correction for convection was based upon average properties between the liquid surface and the flame around the droplet. Analysis was also completed for the open loop response of monopropellant droplets, based upon earlier strand combustion results. At the limit of large droplets, where the effect of flame curvature is small, the results suggest sufficient response to provide a viable mechanism for combustion instability in the frequency and droplet size range appropriate to practical combustors. Calculations are still in progress for a broader range of droplet sizes, including conditions where active combustion effects are small. |
| File Size | 1262461 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750012423 |
| Archival Resource Key | ark:/13960/t6xw96884 |
| Language | English |
| Publisher Date | 1974-01-01 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Fuel Combustion Combustion Physics Monopropellants Combustion Stability Vapor Phases Combustion Products Gasification Burning Rate High Pressure Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |