Three similar twin-engine general-aviation airplane specimens were crash tested at the Langley Impact Dynamics Research Facility at 27 m/sec, a flight-path angle of -15deg, and pithch angles of -15deg, 0deg, and 15deg. 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 Test at Three Pitch Angles
1979-11-01
Audiovisuelles Material
Keine Angabe
Englisch
Light airplane crash tests at three pitch angles
NTRS | 1979
|Light airplane crash tests at three pitch angles
TIBKAT | 1979
|Light Airplane Crash Tests at Three Pitch Angles
NTIS | 1979
|Light Airplane Crash Tests at Three Roll Angles
NTIS | 1979
|Light airplane crash tests at three roll angles
TIBKAT | 1979
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