Two similar general aviation airplanes were crash tested at the Langley impact dynamics research facility at velocities of 13 and 27 m/sec. Other flight parameters were held constant. The facility, instrumentation, tests specimens, and test method are briefly described. Structural damage and accelerometer data are discussed.
Light Airplane Crash Tests at Impact Velocities of 13 and 27 M/Sec
1977
52 pages
Report
Keine Angabe
Englisch
Light Airplane Crash Tests at Three Roll Angles
NTIS | 1979
|Light airplane crash tests at three pitch angles
NTRS | 1979
|Light airplane crash tests at three roll angles
TIBKAT | 1979
|