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Combustion stability with baffles, absorbers and velocity sensitive combustion. [liquid propellant rocket combustors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mitchell, C. E. |
| Copyright Year | 1980 |
| Description | Analytical and computational techniques were developed to predict the stability behavior of liquid propellant rocket combustors using damping devices such as acoustic liners, slot absorbers, and injector face baffles. Models were developed to determine the frequency and decay rate of combustor oscillations, the spatial and temporal pressure waveforms, and the stability limits in terms of combustion response model parameters. |
| File Size | 317435 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800009863 |
| Archival Resource Key | ark:/13960/t9w13w43t |
| Language | English |
| Publisher Date | 1980-02-01 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Damping Green's Functions Combustion Stability Baffles Pressure Oscillations Pressure Distribution Mathematical Models Liquid Propellant Rocket Engines Combustion Chambers Propellant Combustion Nonlinear Systems 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 |
