Realistic helicopter design criteria benefits the operational capability of helicopters by reducing the possibility of over or under design. Better performance and reliability are possible while achieving increased operational availability and reduced maintenance requirements when design criteria reflect more truly the actual operational conditions of significance in establishing design criteria in a realistic mission load spectra. Helicopter loads programs have proceeded along three complementary lines: loads prediction techniques, mission spectrum development, and loads measurement. The results of this effort are currently being used to construct mission profiles for the next generation designs for these aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Helicopter Operational Loads Spectrum and Design Criteria


    Beteiligte:

    Erscheinungsdatum :

    1974


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Criteria for Externally Suspended Helicopter Loads

    S. J. Briczinski / G. R. Karas | NTIS | 1971


    Helicopter sling loads

    Shaughnessy, J. D. / Yenni, K. R. / Deaux, T. N. | NTRS | 1980