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.
Light airplane crash tests at three pitch angles
1979-11-01
Report
Keine Angabe
Englisch
Light airplane crash tests at three pitch angles
TIBKAT | 1979
|Light Airplane Crash Tests at Three Pitch Angles
NTIS | 1979
|Light Airplane Crash Test at Three Pitch Angles
NTRS | 1979
|Light Airplane Crash Tests at Three Roll Angles
NTIS | 1979
|Light airplane crash tests at three roll angles
NTRS | 1979
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