Autor: |
Karimov, Z., Shershnev, A., Chekrygina, T., Bogdanov, A., Kaluzhskii, S., Grachev, A. |
Zdroj: |
Refractories; 1991, Vol. 32 Issue 7/8, p369-372, 4p |
Abstrakt: |
The computer experiment from this model gives a clear-cut relation between the fuel flow rate in the annular channel, the design parameters for the combustion chamber, and the combustion-product temperature in the annular space on the one hand and the particle temperatures and velocities in relation to fractional composition and concentration in the air in the central tube on the other. These equations can thus be used with a computer to obtain technological information to control flame jet conditions. [ABSTRACT FROM AUTHOR] |
Databáze: |
Complementary Index |
Externí odkaz: |
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