Theoretical aspects of aero-engine altitude relighting performance

Lefebvre, A. H.

dc.contributor.author	Lefebvre, A. H.
dc.date.accessioned	2015-10-07T08:32:04Z
dc.date.available	2015-10-07T08:32:04Z
dc.date.issued	1968-03
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/9561
dc.description.abstract	The purpose of this note is to review some current theories of ignition in stagnant and flowing mixtures, and to present an alternative theory to describe the process that occurs in a turbojet combustion chamber when the engine is being relighted after a flame-out at high altitudes.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.relation.ispartofseries	152	en_UK
dc.relation.ispartofseries	COA/M-152	en_UK
dc.title	Theoretical aspects of aero-engine altitude relighting performance	en_UK
dc.type	Report	en_UK