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Combustion instability with partial length acoustic liners
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jotiban, Y. Baer, M. R. Mitchell, C. E. |
| Copyright Year | 1975 |
| Description | The development is discussed of analytical techniques and numerical methods for the prediction of the stability behavior of liquid propellant rocket combustors with partial length acoustic liners, injector face baffles, and nonlinear combustion responses. Three primary objectives included: (1) extension of the Green's Function integral-iteration technique previously developed so that nonlinear three dimensional wave propagation effects could be included in stability predictions; (2) development of an analytical technique and a computer program for the prediction of the damping effects caused by injector face baffles; and (3) inclusion of a nonlinear, wave distortation dependent, combustion response model in the global stability analysis and determination of its effect on combustor stability. |
| File Size | 544097 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760007124 |
| Archival Resource Key | ark:/13960/t3kx05w98 |
| Language | English |
| Publisher Date | 1975-12-01 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Numerical Analysis Wave Propagation Green's Functions Rocket Linings Combustion Stability Liquid Propellant Rocket Engines Combustion Chambers Prediction Analysis Techniques Computer Programs 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 |
