The University of Kansas, Flight Research Laboratory is developing an interactive, user-friendly computer program to perform preliminary design and analysis functions for fixed wing airplanes. This paper presents a discussion of the current status of this program. Use of the program is illustrated with an example application to an advanced stealth bomber.


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    Title :

    Automated Aircraft Configuration Design and Analysis


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    General Aviation Aircraft Meeting and Exposition ; 1989



    Publication date :

    1989-04-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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