Shock-absorbing system of main landing gear must function under impact of landing and while taxiing on landing fields; present requirements for impact landing; typical analysis made to check up proposed system for given airplane; tail-wheel shock-absorber system. (See also - discussion p 327-30)


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    Titel :

    Airplane landing-gear shock-absorbing system


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Johnson, C.V. (Autor:in)


    Erscheinungsdatum :

    1934


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    The Airplane Landing-Gear Shock-Absorbing System

    Johnson, C. V. | SAE Technical Papers | 1934


    Shock-absorbing system of airplane landing gear

    Callerio, P. | Engineering Index Backfile | 1940


    Airplane landing gear

    Maiorca, Salvatore | TIBKAT | 1931


    Airplane landing gear

    Maiorca, S. | Engineering Index Backfile | 1931


    AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

    URBINATI SIMONE / HILLIARD MATT / SMITH JON | Europäisches Patentamt | 2018

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