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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    Title :

    Airplane landing-gear shock-absorbing system


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1934


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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    AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

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    Free access