Abstract In the framework of designing vibration tests for the airborne equipment units the types of fatigue curves of their elements are determined. A method for recounting the value of the specified unit service life with regard for only vibration effect is proposed. Variants of vibration strength bench tests are considered.


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    Title :

    Designing vibration strength tests of flight vehicle airborne equipment


    Contributors:

    Published in:

    Publication date :

    2009-06-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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