The Decision Support Problem (DSP) technique for aircraft design is presently demonstrated through the development of a compromise DSP template for the conceptual design of subsonic transport aircraft. System variables are wing span and area, fuselage diameter and length, takeoff weight, and installed thrust. Such system constraints as range and wing loading are represented algebraically using standard subsonic aircraft theory, and economic efficiency is modeled in terms of rates-of-return. The DSP template thus obtained has been tested and validated using the known mission requirements and design constants of the B 727-200 airliner.


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    Title :

    Compromise - An effective approach for conceptual aircraft design


    Contributors:

    Publication date :

    1987-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Compromise: An effective approach for conceptual aircraft design

    Marinopolous, S. / Jackson, D. / Shupe, J. et al. | Tema Archive | 1987




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