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Development of a Dynamic Aircraft Seat Analysis Capability
ISSN: 0148-7191, e-ISSN: 2688-3627
Published September 11, 2001 by SAE International in United States
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The development of a dynamic aircraft seat analysis is presented in this paper. This analytical model is a nonlinear finite element model composed of a seat frame and cushion, restraint system, glare shield and a rigid body model of a 50th percentile Hybrid-II anthropomorphic test dummy (ATD) occupant. Results from this analytical model are correlated with empirical results obtained during a full-scale dynamic test. The analysis is representative of the dynamic test.
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CitationHermann, T., Holmes, M., and Hartley, D., "Development of a Dynamic Aircraft Seat Analysis Capability," SAE Technical Paper 2001-01-2660, 2001, https://doi.org/10.4271/2001-01-2660.
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