Structural response predictions have been made for two important areas of STOL-type aircraft. The method was developed to significantly improve environmental prediction methods that have been used in the past. A mathematically rigorous spectral analysis approach was developed that simulated the structure with a finite element model and used correlated and calculated acoustic input data for the forcing function. (Author)


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    Titel :

    STOL Aircraft Structural Vibration Prediction Method. Volume 2. Acoustic Prediction Details and Additional Plots for Small STOL Aircraft


    Beteiligte:
    C. S. Doherty (Autor:in) / L. M. Butzel (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    186 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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