EPR is a ratio of
- P4 to P1
- Pfan to P1
- P6 to P1
Explanation from PART66Online
Engine pressure ratio is the total pressure at the turbine discharge, in the jet pipe just behind the last turbine stage, divided by the total pressure at the engine inlet. In this figure the inlet is station 1 and the jet pipe behind the turbine is station 6, so EPR is the ratio of P6 to P1. Station 4 is the turbine inlet, ahead of the turbine, and a straight turbojet like this has no fan, so neither P4 nor a fan pressure is used.
sauravkatwal asked · 16 Feb 2013
WRONG ANSWER!!!!!!
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