Abstract
A comparison of the characteristics of the boundary layer with combustion with flame stabilization by a rib and a backward-facing step is performed. Data on the thermal boundary layer, the flame blow-off velocity, and the rate of ethanol evaporation into an air flow with a turbulence intensity of up to 26% are obtained. It is shown that the temperature of the outer region of the boundary layer and the flame blow-off velocity behind the rib are higher than those behind the backward-facing step. With both methods of flame stabilization, the intensity of evaporation corresponds to transient mass transfer.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.