Combustion instabilities in liquid rocket engines testing and development practices in Russia /
Tallennettuna:
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| Yhteisötekijä: | |
| Muut tekijät: | , , |
| Aineistotyyppi: | Elektroninen E-kirja |
| Kieli: | englanti |
| Julkaistu: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
c2007.
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| Sarja: | Progress in astronautics and aeronautics.
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| Aiheet: | |
| Linkit: | An electronic book accessible through the World Wide Web; click to view |
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Sisällysluettelo:
- 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.