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Combustion instabilities in liquid rocket engines : testing and development practices in Russia /
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Otros Autores: | , , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
©2007.
|
| Colección: | Progress in astronautics and aeronautics.
|
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Introduction
- Terms and definitions
- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level
- Uncertainty in conversion of propellant to combustion products
- Studies of operating process stability at various stages of combustor development
- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators
- Acoustic study of combustion chamber stability characteristics
- Determination of stability of oscillations from natural disturbances
- Evaluation of LRE process stability by use of artificial pressure disturbances
- Model firing tests for selection of injector head elements
- Estimation of operating process stability from pressure oscillation decrements
- Test results for pulsing liquid-liquid chambers
- Stability of gas-liquid combustion chambers
- Gas-liquid combustion-chamber tests for stability to hard excitation
- Injector head for RD-170 engine combustion chamber
- Stability characteristics of engines with adjustable injectors
- Control of stability in production of the proton engine.