A Novel and Simple Model for Preliminary Aircraft Parameters Selection Using Turbofan Engine Database 2004-01-3399
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.
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. Download Citation
Author(s):
Ricardo Pereira das Neves, Alexandre Osti Fraccaroli, João Roberto Barbosa
Affiliated:
Embraer - Empresa Brasileira de Aeronáutica S.A., ITA - Instituto Tecnológico de Aeronáutica
Pages: 13
Event:
2004 SAE Brasil Congress and Exhibit
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Turbofan engines
Design processes
Aircraft
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