an email newsletter released every 3 weeks highlighting the latest articles, events, technical inquires, and voices from the community
How can combustion efficiency be estimated for a liquid-fueled ramjet with a given combustor length or bulk flow residence time flying in the Mach 2-3 range?
The Defense Systems Information Analysis Center (DSIAC) was asked how combustion efficiency can be estimated for a liquid-fueled ramjet flying in the Mach 2-3 range with a given combustor length or bulk flow residence time. In particular, DSIAC was asked for some sort of data or an empirical/analytical model that has been validated with data, rather than non-computational fluid dynamics solutions, that can be used to predict how performance of a ramjet combustor could change over a range of operating conditions. DSIAC found relevant information that was further augmented with input from the DSIAC community via an Active Inquiry.
Want to find out more about this topic?
Request a FREE Technical Inquiry!