Three similar twin engine general aviation airplanes were crash tested at the Langley impact dynamics research facility at 27 m/sec and at nominal roll angles of 0 deg, -15 deg, and -30 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.
Light Airplane Crash Tests at Three Roll Angles
1979
77 pages
Report
No indication
English
Light airplane crash tests at three roll angles
TIBKAT | 1979
|Light airplane crash tests at three roll angles
NTRS | 1979
|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
|