Three similar twin-engine general aviation airplane specimens were crash tested at an impact dynamics research facility at 27 m/sec, a flight path angle of -15 deg, and pitch angles of -15 deg, 0 deg, and 15 deg. Other crash parameters were held constant. The test facility, instrumentation, test specimens, and test method are briefly described. Structural damage and accelerometer data for each of the three impact conditions are presented and discussed.


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    Title :

    Light airplane crash tests at three pitch angles


    Contributors:

    Publication date :

    1979-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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