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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    Title :

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


    Contributors:

    Publication date :

    1979


    Size :

    186 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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