Non-premixed liquid fuel air flame in a miniature combustor with modified flow aerodynamics
This study determines the effect of flow aerodynamics modification on the combustion characteristics of a new miniature combustor. The n-heptane was injected into the combustor at a flow rate of 1.0 ml/min to 2.5 ml/min, and the airflow rate varied between 7.0 l/min and 20.0 l/min at a successive fu...
Main Authors: | , , , , , , , |
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Format: | Article |
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Taylor and Francis Group
2022
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