Combustion of kerosene in a supersonic stream
| Autor: | C. Bruno, P. K. Tret’yakov |
|---|---|
| Rok vydání: | 1999 |
| Předmět: |
Kerosene
Hydrogen General Chemical Engineering Nuclear engineering Mixing (process engineering) General Physics and Astronomy Energy Engineering and Power Technology chemistry.chemical_element General Chemistry Fuel injection Combustion law.invention Ignition system Fuel Technology chemistry law Vaporization Supersonic speed |
| Zdroj: | Combustion, Explosion, and Shock Waves. 35:245-251 |
| ISSN: | 1573-8345 0010-5082 |
| Popis: | Experiments on the organization of the combustion of kerosene in high-enthalpy supersonic air streams is analyzed. The use of promotor additives, as well as improvements in the atomization process, vaporization, and mixing, do not always facilitate efficient combustion development. The existence of a conversion process is found to have a significant effect on the ignition parameters. The burnup intensity can be ensured by adding hydrogen, and the relative position of the fuel injectors is important in that case. The fundamental role of wave structures in determining the length of the combustion zone in the channel is noted. The integral characteristics of combustion for hydrogen and kerosene are compared. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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