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Category:Axial-compressor gas turbine engines

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This is the current revision of this page, as edited by Andy Dingley (talk | contribs) at 09:49, 24 May 2016 (Created page with 'Turbojet engines or other gas turbines, using axial-flow through a multi-stage compressor. These allow a higher overall pressure ratio than a centrifugal com...'). The present address (URL) is a permanent link to this version.

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Turbojet engines or other gas turbines, using axial-flow through a multi-stage compressor. These allow a higher overall pressure ratio than a centrifugal compressor, but are more complex to design.

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