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Numerical Investigation of Occupant Injury Risks During A Realistic Transport Aircraft Crash ConditionsResearchers at the National Aeronautics and Space Administration (NASA) Langley Research Center (LaRC) have conducted a full-scale crash test of a Fokker F28 MK1000 aircraft to investigate the performance of transport aircraft under realistic crash conditions. This crash test was computationally recreated using finite element (FE) human body models (HBMs) to further explore potential injury risks to occupants and analyze the utilization of HBMs in the aerospace crash environment. The Global Human Body Model Consortium (GHBMC) male 50th percentile occupant detailed model (v6.0) and the Toyota Human Model for Safety (THUMS) male 50th percentile occupant model (v6.1) were selected to be used in the crash simulations.

The HBMs were simulated in conditions matching those of anthropomorphic test device (ATD) experiments included within the aircraft cabin during the crash test. Seven occupant locations within the cabin were simulated utilizing each of the models. The models were positioned in a neutral upright posture with hands resting on the legs and the feet contacting the floor. Head, brain, neck, and lumbar vertebra injury metrics were calculated for all trials. Both HBM models required minor modifications to stabilize these simulations. The GHBMC model required added erosion for six parts while the THUMS model only required one in order to complete the full simulation. The THUMS model, however, required a much smaller timestep for stability and therefore took significantly more computational time. In addition the GHBMC model includes integrated instrumentation while the THUMS model requires development and implementation of instrumentation. Both models predicted 100% injury risk for lumbar vertebra fracture in all test conditions. This prediction was in family with high lumbar load values measured by the ATDs during the crash test. The THUMS model consistently predicted lower injury risks than the GHBMC model in all three other metrics varying depending on the crash pulse. Overall, the THUMS model required less modifications to allow for this study. However, the GHBMC models significantly faster run time and integrated instrumentation make it a more intuitive model for this research.
Document ID
20230014320
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Nate Jones
(Virginia Tech Blacksburg, Virginia, United States)
Costin Untaroiu
(Virginia Tech Blacksburg, Virginia, United States)
Jacob B Putnam
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
October 2, 2023
Publication Date
October 12, 2023
Publication Information
Publication: Safe Symposium
Publisher: SAFE Association
Subject Category
Structural Mechanics
Meeting Information
Meeting: SAFE Association 61st Annual Symposium
Location: Virginia Beach, VA
Country: US
Start Date: October 10, 2023
End Date: October 12, 2023
Sponsors: SAFE Association
Funding Number(s)
WBS: 664817.02.07.03.03.02
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Crashworthiness
Finite Element Modeling
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