Need for full scale inflight verification of subcritical aeroelastic characteristics of advanced aircraft; flight flutter techniques, development of impulsive excitation techniques and suitable ballistic devices as means of exciting structure; response measuring system and data analysis; theoretical subcritical response; comparison of experimental and theoretical results; FJ-4 aircraft development program, and A3J-1 flight program; recommendations.


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    Title :

    Application of impulsive excitation to in-flight vibration testing


    Additional title:

    Aerospace Eng


    Contributors:
    Beals, V.L. (author) / Hurley, S.R. (author)

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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