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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    Titel :

    Light airplane crash tests at three pitch angles


    Beteiligte:

    Erscheinungsdatum :

    1979-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Light airplane crash tests at three pitch angles

    Vaughan, Victor L. / Alfaro-Bou, Emilio | TIBKAT | 1979


    Light Airplane Crash Tests at Three Pitch Angles

    V. L. Vaughan / E. Alfaro-bou | NTIS | 1979


    Light Airplane Crash Test at Three Pitch Angles

    Vaughan, Victor L., Jr. / Alfaro-Bou, Emilio | NTRS | 1979


    Light Airplane Crash Tests at Three Roll Angles

    C. B. Castle / E. Alfaro-bou | NTIS | 1979


    Light airplane crash tests at three roll angles

    Castle, C. B. / Alfaro-Bou, E. | NTRS | 1979