Development of a 3-year-old child head–neck finite element model and derivation of novel head injury criterion

2013 ◽  
Vol 19 (3) ◽  
pp. 233-243 ◽  
Author(s):  
F. Meyer ◽  
C. Deck ◽  
R. Willinger ◽  
P. Meyer
Keyword(s):  
Finite Element ◽  
Head Injury ◽  
Finite Element Model ◽  
Element Model ◽  
Head Injury Criterion ◽  
Head Neck

scholarly journals Comparison of control strategies for the cervical muscles of an average female head-neck finite element model

2019 ◽  
Vol 20 (sup2) ◽  
pp. S116-S122 ◽  
Author(s):  
I Putu A. Putra ◽  
Johan Iraeus ◽  
Robert Thomson ◽  
Mats Y. Svensson ◽  
Astrid Linder ◽  
...  
Keyword(s):  
Finite Element ◽  
Finite Element Model ◽  
Control Strategies ◽  
Element Model ◽  
Female Head ◽  
Cervical Muscles ◽  
Head Neck

626 Simulation of the head impact using a head-neck finite element model

2009 ◽  
Vol 2008.21 (0) ◽  
pp. 465-466
Author(s):  
Akira YAMAOKA ◽  
Yusuke MIYAZAKI ◽  
Sadayuki UJIHASHI ◽  
Jonas A. PRAMUDITA ◽  
Yuichiro SAKAMOTO
Keyword(s):  
Finite Element ◽  
Finite Element Model ◽  
Element Model ◽  
Head Impact ◽  
Head Neck

Dynamic Behavior on Emergency Landing of Light Aircraft with Occupant Restraint System

2012 ◽  
Vol 591-593 ◽  
pp. 2513-2517
Author(s):  
Lin Yin Luo ◽  
Yan Bin He ◽  
Xuan Liu ◽  
Xiao Hu Yao
Keyword(s):  
Finite Element ◽  
Finite Element Model ◽  
Element Model ◽  
Restraint System ◽  
Element Analysis ◽  
Occupant Restraint System ◽  
Head Injury Criterion ◽  
Dynamic Finite Element ◽  
Dynamic Finite Element Analysis ◽  
Safety Design

In the case of aircraft emergency landing, occupants’ safety analysis and research is one of the indispensable links in the verification of airworthiness safety. However, traditional experimental methods is time-consuming, complex and costly, seriously affect the development of new models to market. This paper established a finite element model of the full-size aircraft cockpit according to a certain type of amphibious light aircraft, and adding the dummy and safety belt occupant restraint system finite element model on this basis. In accordance with the requirements of CCAR-23 test conditions, using large dynamic finite element analysis software LS-DYNA numerical simulation was processed to study this aircraft’s emergency landing procedure. This paper investigated the dynamic response of the dummy and head injury criterion (HIC) value etc. The results provide certain reference for aircraft emergency landing safety design.

Head–neck finite element model of the crash test dummy THOR

2004 ◽  
Vol 9 (2) ◽  
pp. 175-186 ◽  
Author(s):  
H Yu ◽  
M B Medri ◽  
Q Zhou ◽  
F P DiMasi ◽  
F A Bandak
Keyword(s):  
Finite Element ◽  
Finite Element Model ◽  
Element Model ◽  
Crash Test ◽  
Crash Test Dummy ◽  
Head Neck

FINITE ELEMENT MODEL OF HUMAN HEAD, NECK AND TORSO FOR ADULT AND 3YO CHILD

2012 ◽  
Vol 45 ◽  
pp. S205 ◽  
Author(s):  
Senad Omerovic ◽  
Ana Stojanović ◽  
Simon Krašna ◽  
Ivan Prebil
Keyword(s):  
Finite Element ◽  
Finite Element Model ◽  
Human Head ◽  
Element Model ◽  
Head Neck
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