Light Airplane Crash Tests at Impact Velocities of 13 and 27 m/sec
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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.
[1] E. Alfaro-Bou,et al. Impact dynamics research facility for full-scale aircraft crash testing , 1976 .
[2] I Irving Pinkel,et al. Seat Design for Crash Worthiness , 1957 .
[3] Dugald O. Black,et al. Accelerations and passenger harness loads measured in full-scale light-airplane crashes , 1953 .