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Validation of a Cessna Engine Compressor Model


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Bardela, Paul-Alexandre, Pageaud, Pierre and Botez, Ruxandra. 20 February 2018. « Validation of a Cessna Engine Compressor Model ». [Research article]. Substance ÉTS.

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The number of aircraft passengers is continuously rising. This increase also signifies an increase in harmful gas emissions. The aeronautical industry is aiming to improve its current engines efficiency in order to reduce these emissions. The improvement of engine efficiency requires more accurate models in order to have a better understanding of the different variables involved. This study is focused on modelling the engine’s compressing elements. The purpose of this study is to model the fan pressure ratio, and the engine pressure ratio for all flight conditions. The data needed to identify the model are gathered from the Research Aircraft Flight Simulator (RAFS) of the Aeronautical Research Laboratory in Active Controls, Avionics and Aeroservoelasticity at ÉTS (LARCASE). Key words: engine, compressor, fan, modelling, flight tests, identification, validation

Item Type: Non-peer reviewed article published in a journal or magazine
Refereed: No
Botez, Ruxandra
Affiliation: Génie de la production automatisée
Date Deposited: 06 Aug 2018 15:07
Last Modified: 28 Feb 2019 20:45

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