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  • 1
    facet.materialart.
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    Light airplane crash tests at three pitch angles (1979)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: 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.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-TP-1481 , L-13051
    Format: application/pdf
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