Simulation of Aircraft Seat Response to a Crash Environment 810612
A new structural analysis method is being developed for incorporation into the seat/occupant model (Program SOM-LA), which is intended for use in evaluating the crashworthiness of aircraft seats. The analytical technique is described, and its capabilities are demonstrated in the simulation of the dynamic test of an actual aircraft seat. Computer simulation results are presented and compared with the test data.
Citation: Coltman, J., Bolukbasi, A., and Laananen, D., "Simulation of Aircraft Seat Response to a Crash Environment," SAE Technical Paper 810612, 1981, https://doi.org/10.4271/810612. Download Citation
Author(s):
J. W. Coltman, A. O. Bolukbasi, D. H. Laananen
Affiliated:
Simula Inc.
Pages: 11
Event:
Business Aircraft Meeting and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Computer simulation
Aircraft
Seats and seating
Simulation and modeling
Crashworthiness
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