Validation of a Cessna Engine Model

Bardela, Paul-Alexandre, Pageaud, Pierre and Botez, Ruxandra. 1 March 2018. « Validation of a Cessna Engine Model ». [Research article]. Substance ÉTS.

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Abstract

Environment is one of the most important concerns in the aerospace industry. Engine efficiency is directly linked to the amount of harmful emissions produced. Modelling of gas turbine engines needs to be improved in order to reduce these emissions. The purpose of this study is to model the engine using two outputs: the thrust, which is the force moving the aircraft forward, and the fuel flow used to produce the thrust. These outputs are modelled as function of three inputs: the Mach number, the altitude and the throttle lever angle. The data needed was acquired using the Research Aircraft Flight Simulator (RAFS) from the Laboratory of Applied Research in Active Controls, Avionics and Aeroservoelasticity (LARCASE). Key words: engine, turbofan, modelling, flight tests, identification, validation

Item Type:	Non-peer reviewed article published in a journal or magazine
Refereed:	No
Professor:	Professor Botez, Ruxandra
Affiliation:	Génie de la production automatisée
Date Deposited:	06 Aug 2018 15:06
Last Modified:	28 Feb 2019 20:42
URI:	https://espace2.etsmtl.ca/id/eprint/17174

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