The development of a computer model designed to aid in the preliminary design analysis of general aviation aircraft is described. This model has interrelated in computerized form, the technical disciplines of configuration design, aerodynamics, propulsion, structural weight and balance, and economics to provide a useful engineering tool for identifying critical design parameters and promising advanced technologies. Both analysis of a given airplane and the design of an airplane to meet specified criteria can be achieved with various levels of input and synthesis complexity. Results of a typical parametric analysis are presented for a turbine-powered, six-place configuration.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computer Aided Parametric Analysis for General Aviation Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Business Aircraft Meeting and Engineering Display ; 1973



    Publication date :

    1973-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English