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About: Overall pressure ratio     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : yago:Whole100003553, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)

Type: yago:Artifact100021939yago:Device103183080yago:Engine103287733yago:GasTurbine103426574yago:HeatEngine103507963yago:Instrumentality103575240yago:Internal-combustionEngine103579982yago:Machine103699975yago:Motor103789946yago:Object100002684yago:PhysicalEntity100001930yago:WikicatGasTurbinesyago:RotaryEngine104110654yago:Turbine104498523yago:Whole100003553 New Facet based on Instances of this Class

In aeronautical engineering, overall pressure ratio, or overall compression ratio, is the ratio of the stagnation pressure as measured at the front and rear of the compressor of a gas turbine engine. The terms compression ratio and pressure ratio are used interchangeably. Overall compression ratio also means the overall cycle pressure ratio which includes intake ram.