Subroutines for determining the weights of propulsion system related components and the airframe components of an aircraft configuration are presented. Subroutines that deal with design load conditions, aircraft balance, and tail sizing are included. Options for turbine and internal combustion engines are provided.


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    Titel :

    GASP- General Aviation Synthesis Program. Volume 5: Weights. Part 1: Theoretical Development


    Beteiligte:
    D. Hague (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    168 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch