Combining dynamic loading in laboratory with brittle lacquer stress analysis stated to be quickest method of developing lighter and longer life wheels and brakes; strain in coating and in metal must be considered separately; problem is to obtain Stresscoat pattern exactly at peak of strain magnitude so that direction of strain at its maximum value may be determined; strain gage indicates complete strain cycle.


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    Titel :

    Experimental determination of strains in aircraft landing wheels and brakes


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Polzin, M.H. (Autor:in)


    Erscheinungsdatum :

    1947


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Wheels, Brakes, and Landing Gear

    Filburn, Thomas | Springer Verlag | 2019


    Aircraft wheels and brakes

    Wright, J. | Engineering Index Backfile | 1951


    Aircraft wheels and brakes

    Engineering Index Backfile | 1946


    Landing brakes for aircraft

    Engineering Index Backfile | 1927