Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. (Author)


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    Title :

    Helicopter External Sling System Basic Vibration Data


    Contributors:

    Publication date :

    1969


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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