The study was conducted to determine the dynamic effects of a helicopter external load combination by simulating flight using a computer. Design criteria for sling members and hard points of the system were also established. A computerized hybrid simulation of the coupled motion of a CH-54 helicopter and selected external loads was conducted in real time with a pilot in the loop on both fixed-base and moving-base simulators. The results of the study indicate that the dynamic load factors produced in sling elements and at hard points during a maneuver often exceed the normal load factor developed by the helicopter. Data is included for the various loads and maneuvers.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Criteria for Externally Suspended Helicopter Loads


    Beteiligte:
    S. J. Briczinski (Autor:in) / G. R. Karas (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    210 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Development of Handling Qualities Criteria for Rotorcraft with Externally Slung Loads

    Hoh, Roger H. / Heffley, Robert K. / Mitchell, David G. | NTRS | 2006


    DEVELOPMENT OF HANDLING QUALITIES CRITERIA FOR ROTORCRAFT WITH EXTERNALLY SLUNG LOADS

    Hoh, R. H. / Heffley, R. K. / American Helicopter Society | British Library Conference Proceedings | 2002