The report describes a 'lumped mass' computer simulation of a trailing wire system towed by an orbiting aircraft. The USAF U-10 aircraft flight conditions were used as applied to three flightpaths: constant altitude circular, constant altitude elliptical, and non-constant altitude circular orbit. These flightpaths were flown in no wind and 30 knot wind conditions. Wire lengths of 4000 ft and 8000 ft were used where the free end was attached to a circular sphere of 25 and 100 lbs. The results from 12 orbiting trailing wire configurations are tabulated and/or plotted. One of the main objectives in this analysis was to determine how yo-yo of the free end of the wire in wind might be alleviated or at least minimized. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Dynamics of Cables Towed from Aircraft


    Beteiligte:
    J. G. R. Hansen (Autor:in) / S. A. Crist (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    93 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hydrodynamic Resistance of Towed Cables

    Young-Il Choc / Mario J. Casarella | AIAA | 1971


    Transverse Motion of Towed Cables

    Ersdal, S. / Faltinsen, O.M. | British Library Conference Proceedings | 2006


    Towed aircraft

    Engineering Index Backfile | 1942