In addition to being able to absorb impact equivalent to free fall of aircraft of 27 in., undercarriage must have good taxiing characteristics, must be light in weight, take up as little space as possible, and must have simple retraction arrangement; extensive laboratory tests have resulted in development of number of undercarriages to meet these requirements better, each of which is discussed. (Trans) (See also - discussion p 183, 192)


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    Titel :

    Research and tomorrow's aircraft undercarriage


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Brown, R.W. (Autor:in)


    Erscheinungsdatum :

    1945


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    RESEARCH and Tomorrow's AIRCRAFT UNDERCARRIAGE

    BROWN, ROY W. | SAE Technical Papers | 1945


    "Aircraft Undercarriage"

    Scoles, J. J. / Canadian Aeronautics and Space Institute | British Library Conference Proceedings | 1997


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