Computational modeling and performance evaluation of a DAX-foam aircraft seat cushion utilizing high loading rate dynamic characteristics

Pages: 667 - 674
Published: Jan 1, 2010
Abstract
The aircraft seat dynamic performance standards as per CFR 14 FAR Part 23, and 25 requires the seat to demonstrate crashworthy performance as evaluated using two tests namely Test-I and Test-II conditions. Test-I dynamic test includes a combined vertical and longitudinal dynamic load to demonstrate the compliance of lumbar load requirement for a Hybrid II or an FAA Hybrid III Anthropomorphic Test Device (ATD). The purpose of this test is to...
Paper Details
Title
Computational modeling and performance evaluation of a DAX-foam aircraft seat cushion utilizing high loading rate dynamic characteristics
Published Date
Jan 1, 2010
Journal
Pages
667 - 674
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