Three similar twin engine general aviation airplane specimens were crash tested at Langley impact dynamics research facility at 27 m/sec and at flight-path angles of -15 deg, -30 deg, and -45 deg. Other flight 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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    Titel :

    Light airplane crash tests at three flight-path angles


    Beteiligte:
    Castle, C. B. (Autor:in) / Alfaro-Bou, E. (Autor:in)

    Erscheinungsdatum :

    01.06.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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