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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    Title :

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


    Contributors:
    D. Hague (author)

    Publication date :

    1978


    Size :

    168 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English