This report gives the operator of the Hewlett-Packard (HP-41) handheld calculator the ability to quickly and accurately determine the power requirements of a helicopter in the preliminary design phase. These power requirements are computed for three landing gear configurations: skid, fixed wheel, and retractable wheel. By comparing the power required for each configuration, the user can determine the optimum landing gear for the design.


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    Titel :

    Computer program for preliminary helicopter design


    Weitere Titelangaben:

    Rechnerprogramm fuer eine vorlaeufige Hubschrauberkonstruktion


    Beteiligte:
    Rogers, M.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    126 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    HELICOPTER PRELIMINARY DESIGN

    Landers, C. L. / Lucero, L. / Henthorn, K. D. et al. | British Library Conference Proceedings | 2000


    Helicopter preliminary design

    Landers, Charles L. / Lucero, Luis / Henthorn, Kevin D. | TIBKAT | 2001


    HELICOPTER PRELIMINARY DESIGN

    Landers, C. L. / Lucero, L. / Henthorn, K. D. et al. | British Library Conference Proceedings | 2000