Theoretical aspects of aero-engine altitude relighting performance

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dc.contributor.authorLefebvre, A. H.
dc.date.accessioned2015-10-07T08:32:04Z
dc.date.available2015-10-07T08:32:04Z
dc.date.issued1968-03
dc.description.abstractThe 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/9561
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseries152en_UK
dc.relation.ispartofseriesCOA/M-152en_UK
dc.titleTheoretical aspects of aero-engine altitude relighting performanceen_UK
dc.typeReporten_UK

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