Autor: |
Egorov, A. G., Tizilov, A. S. |
Zdroj: |
Russian Aeronautics; Jun2024, Vol. 67 Issue 2, p378-385, 8p |
Abstrakt: |
The flame stabilization mechanism was implemented in the flow of pseudoliquid fuel through an axisymmetric channel with sudden expansion. Relationships between the flame blow-off velocity and flame stabilization limits were established based on the channel geometric parameters and initial characteristics of the flow of aluminum aerosol particles. Dependencies of flame blow-off velocity in the flow of aluminum aerosol particles ASD-1 and ASD-4 over a wide range of air-fuel ratio variations were obtained. [ABSTRACT FROM AUTHOR] |
Databáze: |
Complementary Index |
Externí odkaz: |
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