The effect of combustor outlet temperature profiles on ramjet thrust

Williams, M. R.; Greenwood, S. W.

dc.contributor.author	Williams, M. R.
dc.contributor.author	Greenwood, S. W.
dc.date.accessioned	2017-03-01T12:08:30Z
dc.date.available	2017-03-01T12:08:30Z
dc.date.issued	1957-07
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/11520
dc.description.abstract	The desirability of obtaining an even distribution of temperature at the outlet of a ramjet combustor is indicated theoretically. Results of experiments on a particular combustion system over a limited range of conditions using a series of mixers are presented. The results suggest that mixers are desirable for high Mach Number ramjets operating at low overall fuel-air ratios. The material presented in this report is based on the work carried out by M. R. Williams in partial fulfilment of the requirements for the Diploma of the College of Aeronautics, and is essentially a summary of his thesis. The work was part of M.O.S. Research Contract 7/Exptl./720	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.relation.ispartofseries	CoA/N-59	en_UK
dc.relation.ispartofseries	59	en_UK
dc.title	The effect of combustor outlet temperature profiles on ramjet thrust	en_UK
dc.type	Report	en_UK