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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    Title :

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


    Additional title:

    Sae Technical Papers



    Conference:

    2004 SAE Brasil Congress and Exhibit ; 2004



    Publication date :

    2004-11-16




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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