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Rowan University

Finite element modeling of a commuter category aircraft seat under crash loading

Abstract

dc:description.abstract

<p>This thesis describes the development and validation of a finite element model of a commuter aircraft seat under crash loading. In particular, this effort has developed an LS-DYNA model of a Beechcraft 1900C low back passenger seat.</p> <p>Although air travel is one of the safest forms of transportation, crash-related fatalities do occur even in relatively low severity crashes. Many of these fatalities can be traced to the inability of production seats to absorb crash energy. The goal of this research effort is to develop a computational model of a production aircraft seat as a first step towards the development of more crash-survivable aircraft seats.</p> <p>The processes by which a finite element model of a low seat-back version of a Beechcraft 1900C passenger seat was created and tested are described in detail. The Beechcraft seat was thoroughly analyzed, a solid model was constructed using the SolidWorks modeling tool, and a mesh model was built from the solid model using the HyperMesh code.</p> <p>The model was first validated against the results of three drop tests conducted in the Rowan drop tower. The model was then validated against a full fuselage drop test of a Beechcraft 1900C, conducted by the FAA. The model was shown to be an excellent predictor of pelvic acceleration. Reasonable agreement was observed between numerical simulation and experiment for all tested body regions; pelvic, chest, and head body regions. With further refinement, the model will serve as a promising computational tool for the future development of energy absorbing aircraft seats.</p>

Degree

thesis:*
Name thesis:degree_name
M.S. in Engineering
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Mechanical Engineering
Year dc:date.available
2003

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Bowen, David William
Contributors dc:contributor
  • Gabler, Hampton C.

Subjects

dc:subject × 2

Identifiers

dc:identifier.*
Repository record dc:identifier
https://rdw.rowan.edu/etd/1261
OAI identifier oai:identifier
oai:rdw.rowan.edu:etd-2261

Chain of custody

source
Harvested from
Rowan University
Base URL
rdw.rowan.edu/do/oai/
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
citation

Bowen, David William. Finite element modeling of a commuter category aircraft seat under crash loading. Thesis thesis, 2003. https://rdw.rowan.edu/etd/1261