A description is given of various loading systems used for the laboratory simulation of the loading environment encountered by aircraft during its operational service. Particular attention is paid to the electrohydraulic servovalve loading system because of its increasing use in structural testing, and reference is made to the problems of multichannel loading systems and to the cost of such systems. (Biller)


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    Title :

    Loading systems for aircraft structural testing


    Additional title:

    Belastungsmethoden fuer die Pruefung von Flugzeug-Bauteilen


    Contributors:


    Publication date :

    1976


    Size :

    15 Seiten, 7 Bilder, 3 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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