Measurements were made of `impact factors' for 89×25×43 cm aircraft wheel rolling over selection of airfield landing lights; impact factors is defined as maximum dynamic load due to impact with landing light divided by normal load prior to impact; wooden models were used to simulate shapes of landing lights and change in load was measured at different speeds on strain gaged axle of test wheel of heavy load vehicle. (39161)


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    Titel :

    Tyre impact tests on airport landing lights


    Weitere Titelangaben:

    Gt Brit, Min Transp, Road Res Lab, Road Res Tech, RRL Rep


    Beteiligte:
    Williams, T. (Autor:in)


    Erscheinungsdatum :

    1968


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Aeroplane landing lights

    Calvert, E.S. | Engineering Index Backfile | 1938


    Aeroplane landing lights

    Calvert, E.S. | Engineering Index Backfile | 1938


    Aeroplane Landing Lights

    Calvert, E.S. | Emerald Group Publishing | 1938


    Landing and taxing tests over various types of runway lights

    Dreher, Robert C / Batterson, Sidney A | NTRS | 1958