Development of a Dynamic Aircraft Seat Analysis Capability

2001-01-2660

09/11/2001

Event
Advances In Aviation Safety Conference & Exposition
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/2001-01-2660
Pages
8
Citation
Hermann, 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.
Additional Details
Publisher
Published
Sep 11, 2001
Product Code
2001-01-2660
Content Type
Technical Paper
Language
English