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Back to: "E"engine pressure ratio
- Definição1
- The ratio of turbine discharge pressure divided by compressor inlet pressure, which is used as an indication of the amount of thrust being developed by a turbine engine.
- Fonte1
- FEDERAL AVIATION ADMINISTRATION. Pilot's handbook of aeronautical knowledge. [s.l.], 2008. Disponível em http:// www.faa.gov/regulations_policies/handbooks_manuals /aviation/pilot_handbook/media/PHAK %20-%20Cover-Preface.pdf. Acesso em: 26 jun. 2014.
- Fonte2
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Environmental technical manual: procedures for the emissions certification of aircraft engines. 2.ed. Volume 2. Montreal, 2014. (Doc. 9501)
- Fonte3
- EMBRAER. Technical dictionary english-portuguese. [São José dos Campos], 2001.
- Nota adicional1
- Acronym in English: EPR.
- Contexto
- Engine pressure ratio and corrections to standard day may be based on the validated engine performance model that is used to represent the reference engine.
- Subárea1
- Engine
- Português
- razão de pressão do motor