A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database

Paper #:
  • 2004-01-3399

Published:
  • 2004-11-16
Citation:
das Neves, R., Fraccaroli, A., and Barbosa, J., "A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database," SAE Technical Paper 2004-01-3399, 2004, https://doi.org/10.4271/2004-01-3399.
Pages:
13
Abstract:
Aircraft engine selection is an important part of both the design process of a new aircraft and the re-powering of an existing aircraft.This paper is a step further on Svoboda's [1] turbofan engine database as a preliminary design tool, aiming at a novel and simple tool for turbofan engine selection during the preliminary aircraft parameters definition, as well as at evaluating current configurations and identifying future trends for the turbofan engines.
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