Motorcycle helmets are vital to protect from recurrent road accidents as they prove crucial in reducing brain trauma. This research piece presents a new and plausible bio-inspired design affined to the foam liner material and structure in helmets. The proposed liner design is inspired from animal horn micro-structure and tubule arrangement. An innovative drop-testing apparatus is presented with a spring-ratchet mechanism for experimental testing. The aim is to validate the new design by meeting the ECE 22.05 standard for motorbike helmets using peak linear acceleration and HIC criteria. Experimental results are partly verified against FEA simulations for two proposed samples. Further samples call for more complex simulations at a later stage to best describe material properties and structures.
The document discusses the social media campaign for the movie The Hunger Games. It details the timeline of the campaign beginning in March 2011 with casting announcements on Facebook. It describes the various social media platforms used including Facebook, Twitter, Tumblr and YouTube. It provides metrics on the success of the campaign, noting it generated over 3 million conversations and had the 3rd highest opening weekend for a non-sequel, bringing in $152.2 million. The campaign budget was smaller than typical at $45 million but was more focused on social media.
1) The document analyzes the structural response of an aircraft fuselage stiffened panel through finite element modeling and analysis.
2) Key aspects analyzed include modeling different stiffener configurations, determining stresses and deformations under various loads, and identifying critical locations.
3) Results show the panel with I-stringers has the least deformation. Buckling analysis identified a critical buckling stress. Stress near mouse holes increases with their height. Maximum stresses at rivet holes were below the material yield strength.
Design & Analysis of Composite Propeller ShaftIJSRD
A Propeller Shaft is the connection between the transmission and the rear axle of the vehicles. The function of propeller shaft is to transmit the power from engine to the rear wheel in case of front engine drive vehicle. High quality steel (Steel SM45) is most commonly used material. The steel drive shaft consists of three universal joints, a center supporting bearing and a bracket, which increase the total weight of a system. The Power transmission can be improved through reducing its weight. According to previous researches many have done the various experiments to reduce the weight by changing the ply thickness, fiber orientation angle, number of plies but until now no one has studied the effect on the properties of the composite formed by changing volume fraction of carbon fiber & epoxy resin. The focus of this work will be to investigate either replacing steel structure of propeller shaft by composite structure such as carbon fiber & epoxy resin to minimize the cost and weight, also to check the suitability of composite structures by experimental method and software testing.
This document describes a finite element based micromechanics model to predict the stress relaxation behavior of woven fabric composites. The model represents the woven fabric as a repeating unit cell with viscoelastic tows embedded in a matrix. Properties of the constituents are determined through experiments and micromechanical modeling. The unit cell model is verified against experimental flexural tests. Stress distributions within the model agree with experiments over time, capturing the stress relaxation behavior of the composite. The model provides an accurate way to predict stress relaxation without extensive material testing.
This document discusses alternative lightweight materials and manufacturing technologies for vehicle frontal bumper beams. Three composite materials - GMT, GMTex, and GMT-UD - were characterized and evaluated through testing for their potential use in bumper beams. Quasi-static tensile, compression, and impact tests were conducted to determine the materials' mechanical properties and impact performance. Finite element analysis was also used to simulate impact loading and compare the performance of the composite materials to existing steel solutions. The results indicate the composite materials, especially GMT-UD, could provide advantages over steel in energy absorption and weight reduction while maintaining sufficient strength and stiffness for the bumper beam application.
The document discusses the social media campaign for the movie The Hunger Games. It details the timeline of the campaign beginning in March 2011 with casting announcements on Facebook. It describes the various social media platforms used including Facebook, Twitter, Tumblr and YouTube. It provides metrics on the success of the campaign, noting it generated over 3 million conversations and had the 3rd highest opening weekend for a non-sequel, bringing in $152.2 million. The campaign budget was smaller than typical at $45 million but was more focused on social media.
1) The document analyzes the structural response of an aircraft fuselage stiffened panel through finite element modeling and analysis.
2) Key aspects analyzed include modeling different stiffener configurations, determining stresses and deformations under various loads, and identifying critical locations.
3) Results show the panel with I-stringers has the least deformation. Buckling analysis identified a critical buckling stress. Stress near mouse holes increases with their height. Maximum stresses at rivet holes were below the material yield strength.
Design & Analysis of Composite Propeller ShaftIJSRD
A Propeller Shaft is the connection between the transmission and the rear axle of the vehicles. The function of propeller shaft is to transmit the power from engine to the rear wheel in case of front engine drive vehicle. High quality steel (Steel SM45) is most commonly used material. The steel drive shaft consists of three universal joints, a center supporting bearing and a bracket, which increase the total weight of a system. The Power transmission can be improved through reducing its weight. According to previous researches many have done the various experiments to reduce the weight by changing the ply thickness, fiber orientation angle, number of plies but until now no one has studied the effect on the properties of the composite formed by changing volume fraction of carbon fiber & epoxy resin. The focus of this work will be to investigate either replacing steel structure of propeller shaft by composite structure such as carbon fiber & epoxy resin to minimize the cost and weight, also to check the suitability of composite structures by experimental method and software testing.
This document describes a finite element based micromechanics model to predict the stress relaxation behavior of woven fabric composites. The model represents the woven fabric as a repeating unit cell with viscoelastic tows embedded in a matrix. Properties of the constituents are determined through experiments and micromechanical modeling. The unit cell model is verified against experimental flexural tests. Stress distributions within the model agree with experiments over time, capturing the stress relaxation behavior of the composite. The model provides an accurate way to predict stress relaxation without extensive material testing.
This document discusses alternative lightweight materials and manufacturing technologies for vehicle frontal bumper beams. Three composite materials - GMT, GMTex, and GMT-UD - were characterized and evaluated through testing for their potential use in bumper beams. Quasi-static tensile, compression, and impact tests were conducted to determine the materials' mechanical properties and impact performance. Finite element analysis was also used to simulate impact loading and compare the performance of the composite materials to existing steel solutions. The results indicate the composite materials, especially GMT-UD, could provide advantages over steel in energy absorption and weight reduction while maintaining sufficient strength and stiffness for the bumper beam application.
Static Structural, Fatigue and Buckling Analysis of Jet Pipe Liner by Inducin...IRJET Journal
This document analyzes the static structural, fatigue, and buckling behavior of conventional and corrugated jet pipe liners through finite element analysis. A conventional liner model and optimized corrugated liner model were created and meshed. Static structural analysis found that the corrugated liner had lower deformation and similar von-Mises stresses to the conventional liner. Fatigue analysis determined the corrugated liner had a slightly lower fatigue life but still above the design target of 1 million cycles. Buckling analysis revealed the corrugated liner had a higher buckling load multiplier, indicating it is stiffer than the conventional liner against buckling. In conclusion, introducing corrugation improved the liner's buckling strength without negatively impacting other
This document presents a study comparing the fatigue performance of a steel leaf spring and a glass fiber/epoxy composite leaf spring used in automobiles. A finite element model was created of each leaf spring using ANSYS software. Static analysis showed the composite spring had higher stiffness but similar maximum stress compared to the steel spring. Fatigue analysis using the Gerber approach predicted the composite spring would have a longer fatigue life of 1.025*10 cycles compared to the steel spring. The document concludes the composite spring design and simulation validate methods for predicting fatigue performance without full physical testing.
The document discusses the design and analysis of a composite leaf spring. It begins with an abstract that outlines replacing steel leaf springs with composite materials to reduce weight. It then provides sections on leaf springs, composite materials, literature reviews on previous composite leaf spring research, and the project overview which involves designing leaf springs in CATIA and analyzing them in ANSYS. The document provides details on the material properties, design calculations, and modeling and analysis procedures.
1. The document analyzes damage tolerance of a fuselage stiffened panel using finite element analysis. It calculates stress intensity factors for longitudinal cracks initiated at rivet holes under internal pressurization loads.
2. The stress intensity factor is calculated using the modified virtual crack closure integral method for crack lengths from 50mm to 1000mm. The stress intensity factor increases with crack length but decreases when the crack reaches frames.
3. For a crack length of 900mm, the calculated stress intensity factor is below the material's fracture toughness, indicating the design is safe for the analyzed internal pressurization loads.
This document summarizes a study that used finite element analysis to analyze the stress distribution in transfemoral prosthetic sockets made of different materials and geometries. A 3D model of a prosthetic socket was developed and analyzed in Solidworks. Various materials were tested including PEEK, Perlon, and glass fiber. The results showed that a PEEK socket design provided the best results with 94.64% stress reduction compared to other materials. The study aims to identify optimal socket designs that improve comfort and reduce failure rates by better distributing stresses on the residual limb. Future work could involve analyzing different soft tissue and residual limb shapes to make the models and results more applicable.
Finite Element Analysis of Pedal Power Hub dynamomsejjournal
The Hub Dynamos are built for electricity generation form the bicycle motion and they are in light weight
and have low frictional resistance. However they are still subjected to normal bicycle loading such as
bicycle frame, rider weight, acceleration, braking and cornering forces. The challenge is to develop a
lightweight hub housing and hub axle that can safely withstand the required loads. The present paper deals
with designing a Hub dynamo assembly using Solid Works Office Premium software. The assembly
comprises of the Hub shell, hub axle, internal gear assembly, armature, and fasters. Static structural
analysis was done using SW simulation software. The plots for equivalent von-misesstress plot, total
deformation plot were obtained and the design was continuously optimized till a safe design was
obtained.Maximum distortion energy theory was used for the analysis. The material assignment is as
follows: hub assembly- Aluminum Alloys 356.0 T-6, hub axle- ASTM A36 Steel and Gear Assembly
Bracket- Alloy Steel (SS).
FINITE ELEMENT ANALYSIS OF PEDAL POWER HUB DYNAMOmsejjournal
The Hub Dynamos are built for electricity generation form the bicycle motion and they are in light weight
and have low frictional resistance. However they are still subjected to normal bicycle loading such as
bicycle frame, rider weight, acceleration, braking and cornering forces. The challenge is to develop a
lightweight hub housing and hub axle that can safely withstand the required loads. The present paper deals
with designing a Hub dynamo assembly using Solid Works Office Premium software. The assembly
comprises of the Hub shell, hub axle, internal gear assembly, armature, and fasters. Static structural
analysis was done using SW simulation software. The plots for equivalent von-misesstress plot, total
deformation plot were obtained and the design was continuously optimized till a safe design was
obtained.Maximum distortion energy theory was used for the analysis. The material assignment is as
follows: hub assembly- Aluminum Alloys 356.0 T-6, hub axle- ASTM A36 Steel and Gear Assembly
Bracket- Alloy Steel (SS).
FINITE ELEMENT ANALYSIS OF PEDAL POWER HUB DYNAMOmsejjournal
The document summarizes a finite element analysis of a pedal power hub dynamo assembly. A 3D model of the assembly was created in SolidWorks consisting of a hub shell, hub axle, gear assembly bracket, and other parts. Static structural analysis was performed on the hub shell, gear assembly bracket, and hub axle individually. For each part, the material properties were defined, loads and boundary conditions were applied, and the equivalent von-Mises stress and total deformation plots were obtained from the simulation and analyzed. The maximum stresses calculated for each part were significantly lower than the yield strengths of the respective materials, indicating the designed hub dynamo assembly can safely withstand the expected loading conditions.
The document analyzes the free vibration of sandwich beam structures using finite element modeling. Three models are created in MSC PATRAN/NASTRAN software: a 1D beam model, 2D shell model, and 3D solid model. The natural frequencies and mode shapes are calculated for beams made of aluminum (AL), chlorinated polyvinyl chloride (CPVC), and an AL-CPVC sandwich construction beam, under different boundary conditions. The finite element results show good agreement with analytical models for the AL and CPVC solid beams, with less than 2% error. However, for the AL-CPVC sandwich beam, the analytical solution over-predicts the natural frequencies, with errors increasing from 27% for the first
Determination of Buckling Loads of Wave Spring Using ANSYSIJRES Journal
Special performance characteristics are individually built into each spring to satisfy a variety of precise operating conditions. Typically, a wave spring will occupy an externally small area for the amount of work it performs. The present work deals with the structural analysis of wave and coil spring by modeling the structural behavior of these springs using three dimensional finite elements (FE) software. The design of spring in suspension system is very important. In this work a wave type of spring is designed and a 3D model is created using CREO software. The model is also varied by changing the length of the spring. Structural analysis has been conducted on the wave spring by varying thickness and number of turns. For the analysis, loads are bike weight with single and two persons. The buckling load is then estimated for both Wave spring and coil spring with the same parameters.
Prediction of Fatigue Life of Boom Nose End Casting Using Linear Elastic Frac...IJERA Editor
The document discusses predicting the fatigue life of a boom nose end casting used in excavators. It describes performing finite element analysis to determine stresses on the casting under different loads and crack lengths. The results from finite element analysis and a theoretical approach using linear elastic fracture mechanics are then used to estimate the fatigue life of the casting.
IRJET- Optimum Design of a Trailer Chassis to Overcome Failures of Welded Joi...IRJET Journal
1) The document discusses the finite element analysis of a trailer chassis to optimize its design and overcome failures in welded joints.
2) A CAD model of the chassis was created in SolidWorks and imported into ANSYS for finite element analysis to simulate loads and study stress distributions.
3) The analysis found high stresses at welded joints connecting cross members to the main frame, indicating these are failure points. Optimizing the chassis design could improve maintenance needs and reduce costs by extending the lifespan.
Manoj Kumar Kongari is seeking a role in CAE and design. He has over 2 years of experience as a CAE engineer. He holds a B.Tech in Mechanical Engineering and certifications in SolidWorks. His project experience includes structural analysis of various mechanical assemblies and components using FEA tools like ABAQUS and SolidWorks Simulation. He has strong communication, analytical, and teamwork skills.
IRJET- Static and Dynamic Analysis of a Two Wheeler Shock Absorber using ...IRJET Journal
This document presents a study analyzing the static and dynamic performance of a two-wheeler shock absorber using different materials for the helical coil spring. A 3D model of a shock absorber is created in SolidWorks. Structural, modal, frequency response, and transient analyses are performed to evaluate stresses, displacements, natural frequencies, and dynamic response under various loading conditions. Five different materials - stainless steel, carbon steel, phosphor bronze, beryllium copper, and titanium alloy - are considered for the spring. The analyses aim to determine the best material for the spring to improve the shock absorber's performance.
Finite Element Analysis of Connecting rod for Internal Combustion Engines: A ...IRJET Journal
This document reviews research on finite element analysis of connecting rods for internal combustion engines. It discusses how connecting rods transmit forces between the piston and crankshaft. The document summarizes various studies that analyzed connecting rod design, materials, stresses, and optimization using modeling software. It describes how connecting rods can be made of steel, aluminum alloys, or composites and discusses efforts to reduce weight and cost while improving strength and fatigue life through material selection and design optimization. The goal of the research discussed is to better understand connecting rod behavior under dynamic loading and explore opportunities to improve engine performance and efficiency.
Finite Element Analysis of Damping Performance of VEM Materials Using CLD Tec...IJERA Editor
Most engineering structures experiences vibrational motion, this unwanted vibrations can result in premature
structural failure. Many methods are developed which enhances capability of damping such as constrained layer
damping. Shear motion is produced in VEM due to constraining layer to resist unwanted vibrational energy.
This paper shows theeffect of varying the thickness of viscoelastic materials on damping performance of CLD
beam.The damping performance is measured in terms of modal loss factor.
Axial Forces of a Half-spherical Space Truss Structure with OpeningIRJET Journal
1. The document investigates the effect of an opening on the maximum axial forces of a half-spherical space truss structure.
2. Analysis of a regular half-spherical truss model found maximum tension of 523.7 kg and compression of -105.2 kg.
3. Analysis of a half-spherical truss model with an opening found significantly higher maximum tension of 6642.4 kg and compression of -7857 kg, exceeding structural capacity.
4. Replacing members with higher forces with a larger steel profile allowed structural capacity requirements to be met for the model with an opening.
This document summarizes a study on the seismic performance of reinforced concrete (RC) framed structures designed using the partial capacity design (PCD) method. PCD aims to ensure plastic hinges only form at expected locations by designing interior columns for nominal seismic loads and exterior columns for higher seismic loads using a magnification factor formula. The study models 2D and 3D RC frames in SAP software and designs them according to Indian codes using the new magnification factor formula. Nonlinear pushover analysis shows the frames achieve the assumed collapse mechanism as exterior columns remain elastic. Overstrength factors between 1.03-1.21 and magnification factors between 2.35-3.87 are calculated for the frames. The study concludes PCD is effective if exterior column
IRJET- Computational Fluid Dynamic Analysis and Mechanical Strength Evaluatio...IRJET Journal
This document presents a computational fluid dynamic (CFD) analysis and mechanical strength evaluation of additively manufactured customized bone scaffolds. Static structural analysis using finite element analysis was conducted on 3D printed cobalt chrome scaffold models to evaluate mechanical properties under different loads. CFD analysis using ANSYS Fluent was also performed to analyze fluid behavior through the porous scaffold structures when exposed to synovial fluid conditions. The results show that cobalt chrome scaffolds experience lower deformation and equivalent stress compared to titanium scaffolds, indicating better mechanical properties. Fluent analysis results demonstrate variations in streamline velocity and pressure contours through different scaffold designs that mimic natural bone conditions in the human body. The study aims to evaluate scaffold designs for orthopedic implants that are both mechanically
This document describes a minor project to evaluate the effect of fiber orientation on the natural frequency of composite materials. A group of students will conduct experiments using glass fiber-epoxy composite plates fabricated with fiber orientations of 0°, 15°, 30°, 45°, 60°, and 90°. They will use a frequency generator, amplifier, and subwoofer to induce plate vibrations and observe resulting Chladni patterns using granulated wheat. Preliminary results show the natural frequency and mode shapes vary with fiber orientation. The project aims to better understand how fiber orientation impacts composite material properties and dynamic response.
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1. The document analyzes damage tolerance of a fuselage stiffened panel using finite element analysis. It calculates stress intensity factors for longitudinal cracks initiated at rivet holes under internal pressurization loads.
2. The stress intensity factor is calculated using the modified virtual crack closure integral method for crack lengths from 50mm to 1000mm. The stress intensity factor increases with crack length but decreases when the crack reaches frames.
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This document summarizes a study that used finite element analysis to analyze the stress distribution in transfemoral prosthetic sockets made of different materials and geometries. A 3D model of a prosthetic socket was developed and analyzed in Solidworks. Various materials were tested including PEEK, Perlon, and glass fiber. The results showed that a PEEK socket design provided the best results with 94.64% stress reduction compared to other materials. The study aims to identify optimal socket designs that improve comfort and reduce failure rates by better distributing stresses on the residual limb. Future work could involve analyzing different soft tissue and residual limb shapes to make the models and results more applicable.
Finite Element Analysis of Pedal Power Hub dynamomsejjournal
The Hub Dynamos are built for electricity generation form the bicycle motion and they are in light weight
and have low frictional resistance. However they are still subjected to normal bicycle loading such as
bicycle frame, rider weight, acceleration, braking and cornering forces. The challenge is to develop a
lightweight hub housing and hub axle that can safely withstand the required loads. The present paper deals
with designing a Hub dynamo assembly using Solid Works Office Premium software. The assembly
comprises of the Hub shell, hub axle, internal gear assembly, armature, and fasters. Static structural
analysis was done using SW simulation software. The plots for equivalent von-misesstress plot, total
deformation plot were obtained and the design was continuously optimized till a safe design was
obtained.Maximum distortion energy theory was used for the analysis. The material assignment is as
follows: hub assembly- Aluminum Alloys 356.0 T-6, hub axle- ASTM A36 Steel and Gear Assembly
Bracket- Alloy Steel (SS).
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The Hub Dynamos are built for electricity generation form the bicycle motion and they are in light weight
and have low frictional resistance. However they are still subjected to normal bicycle loading such as
bicycle frame, rider weight, acceleration, braking and cornering forces. The challenge is to develop a
lightweight hub housing and hub axle that can safely withstand the required loads. The present paper deals
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comprises of the Hub shell, hub axle, internal gear assembly, armature, and fasters. Static structural
analysis was done using SW simulation software. The plots for equivalent von-misesstress plot, total
deformation plot were obtained and the design was continuously optimized till a safe design was
obtained.Maximum distortion energy theory was used for the analysis. The material assignment is as
follows: hub assembly- Aluminum Alloys 356.0 T-6, hub axle- ASTM A36 Steel and Gear Assembly
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Finite Element Analysis of Damping Performance of VEM Materials Using CLD Tec...IJERA Editor
Most engineering structures experiences vibrational motion, this unwanted vibrations can result in premature
structural failure. Many methods are developed which enhances capability of damping such as constrained layer
damping. Shear motion is produced in VEM due to constraining layer to resist unwanted vibrational energy.
This paper shows theeffect of varying the thickness of viscoelastic materials on damping performance of CLD
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1. The document investigates the effect of an opening on the maximum axial forces of a half-spherical space truss structure.
2. Analysis of a regular half-spherical truss model found maximum tension of 523.7 kg and compression of -105.2 kg.
3. Analysis of a half-spherical truss model with an opening found significantly higher maximum tension of 6642.4 kg and compression of -7857 kg, exceeding structural capacity.
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Towards A Safer Design of Helmets: Finite Element & Experimental Assessment
1. Department of Mechanical Engineering American University of Beirut
Towards a Safer Design of Helmets:
Finite Element and Experimental Assessment
The 2016 ASME
International Mechanical Engineering
Congress & Exposition
Phoenix Convention Center, Phoenix, AZ
November 16, 2016
2. Department of Mechanical Engineering American University of Beirut
Sarah Siblini
Structural Engineer
MEA – Air Liban
Authors & Current
Affiliations
Mutasem Shehadeh, PhD
Associate Professor
American University of Beirut (AUB)
Bilal Wehbi
Graduate Engineer
Petrofac Emirates LLC
Omar Abro
Post-graduate Studies
Imperial College London
Sari Kassar
Rackham Graduate School
University of Michigan
3. Motivation
3
Did you know? Motorcyclists …
➢ More vulnerable to injury than car passengers
➢ Best preventive method of head injury to date motorcycle helmets
➢ Helmet design is effective but not ideal reduces head injury by 72%
Objectives
❖ Improve energy absorption in motorcycle helmet foam liner
❖ Decrease peak linear acceleration and head injury criterion values
❖ Allow helmet to sustain multiple impacts and ensure safety
4. Project Deliverables
① Literature Review
• Biomechanics of Head Injury and Tolerance Limits
• Helmet Anatomy
• Bio-inspired Design
② Experimental Assessment
• Materials Used for Liner
• ISO J Head-Form
• Drop Testing Apparatus
• Tested Samples and Multiple-Impact Results
• Proposed Bio-inspired Sample and Results
③ Finite Element Analysis
• Geometry
• UTM Compression of Cork and EPS
• Material Properties
• Boundary Conditions 4
5. The helmet will be tested based on the ECE 22.05 European standard with PLA
< 275g and HIC < 2400 at impact speed 7.5m/s
Biomechanics of Head Injury and
Tolerance Limits
5
Head Injury
Accounts to higher % among other body parts in fatalities
1. Brain Injury primary “failure” mode
2. Skull Fracture
3. Neck Injury
4. Scalp damage
Head Tolerance Limits and Criteria
1- Peak Linear Acceleration (PLA):
Maximum value of acceleration measured at COG of head-
form i.e. Brain; in units of “g” (gravitational
acceleration=9.81m/s2)
2- Head Injury Criteria (HIC):
Based on Wayne state tolerance curve; takes into account
impact duration Wayne State Tolerance Curve
(Kelvin,2002)
6. Helmet Anatomy
6
The Basic Safety Components of a
Motorcycle Helmet:
1. Outer Shell
2. Liner Foam
3. Visor
4. Fastening Strap
5. Interior Padding
The Expanded Polystyrene (EPS) foam liner:
• Thickness: 30 - 40 mm
• Absorbs the most impact energy of 30-50% (Pinnoji et
al. and Kostopoulos et al.)
• Closed-cell low weight foam, cheap, and undergoes
permanent crushing
7. Bio-Inspired Design
7
Cattle horns, rhinoceros horns, and equine hooves offer great shock
absorbance for linear and rotational impact application
Horn Structure
•Arranged in a lamellar structure of keratin
sheets.
•Lamellar structures are in the radial direction
with tubules (d=40-500 µm) longitudinally.
(8-12% porosity outside and 0% inside)
•Compression in the radial direction has the
lowest elastic modulus and yield strength
allowing for more energy absorbance
Horn Anatomy
Oriented Keratin Fiber Structure
Loaded in Radial Direction
(redrawn from McKittrick et al.)
8. Materials Used for Liner in Testing
8
Micro Agglomerate Cork (MAC)
Acts as a spring, has high elasticity, viscoelastic in
nature but much denser
Expanded Polystyrene (EPS)
Light material, can be modeled as isotropic, one-time
use
Sandwiched Configuration:
A combined structure of Cork-EPS-Cork with MAC
(20-40%) in a linearly packed structure would show
best properties in shock absorption (Coehlo et al.)
9. ISO-J Head form
9
• Made according to ECE 22.05 ISO-J Headform Standard
• High strength aluminum “ALUMEC” of density 2830 kg/m3 and tensile
strength of 575 MPa
• Weighs 4.038kg with accelerometer (SlamStick-X)
• Drawn with CAD software “Rhinocerous”
• CNC manufactured at AUB
Extracted from: http://www.cadexinc.com/en960_full_urethane_headform.php
Plastic SlamStick
Accelerometer by MIDE
Can take 500g and 20KHZ
sampling
11. Drop Testing Apparatus
11
• Spring loaded mechanism
(of stiffness k instead of drop tower)
to reach speed of 7.5m/s
• Heavy bottom base (100kg)
to simulate flat impact and anvil
D=14cm
• The pulling mechanism consists
of a manual ratchet pulley
mechanism that can withstand
2.5 tons
In-House Built Impact Apparatus and
Components
12. Tested Samples
12
Figure: Preliminary Foam Configurations Tested
Sample 1: CEC: MAC Layer- EPS Layer - MAC Layer
Sample 2: CECE: MAC Layer- EPS Layer - MAC Layer -EPS Layer
Sample 3: EPS Only
Sample 4: CE: MAC Layer(top) - EPS Layer
Sample 5: Preliminary Bio-inspired Sample
Sample 6: Enhanced Bio-inspired Sample (covered later)
14. Multi-Impact Results:
CEC and CECE
14
cec impact1
cec impact3
cec impact2
time (ms)
acceleration(g)
Head Impact Curves for Multiple Impact on CEC Configuration
time (ms)
acceleration(g)
Head Acceleration Curves for Multiple Impact on CECE Configuration
cece impact1
cece impact3
cece impact2
260 278Average
15. Multi-Impact Results:
Bio-inspired Design 1
15
time (ms)
acceleration(g)
Head Impact Curves for Multiple Impact on Preliminary Bio-inspired Design
Configuration
biodesign
biodesign
19. Finite Element Analysis
19
EPS Foam Compression Curve Explained (Same for MAC)
Elastomeric forms typically show the following
behavior composed of 3 stages in the figure
(extracted from Di Landro et al.)
Figure : Typical Stress-Strain Diagram of
rigid foam
elastic
Plastic plateau
Densification
(Vaitkus et al.)
EPS microstructure
EPS macrostructure
density 23kg/m3
Stress Strain Curves EPS representative densities
(L Cui. Et al)
20. Finite Element Analysis
- Materials
20
Modeling Cork in ABAQUS
• Quasi-Static compression (strain rate 10mm/s)
• Eight-node brick element with reduced
integration (C3D8R)
• Permanent energy dissipation using the
“Mullins Effect” along with the Hyper-foam
model. (Fernandes et al.)
• Result: 2.4mm deformation (verified)
Modeling EPS in ABAQUS
• Same conditions as above
• “Crushable Foam” in ABAQUS library with
volumetric hardening along with linear
elastic model
• Result: 7.5mm deformation (verified)
Side Note on Modeling ABS:
Literature values of E = 2 GPA v=0.37 , and
yield stress of 60 MPa; elastic and perfectly
plastic(L.T Chang et al.)
21. Finite Element Analysis
Geometry and BC
21
• Geometry of the head-form is imported to ABAQUS for meshing and
introducing material properties (modeled as rigid along with anvil)
• The outer foam liner and shell are drawn with PTC Creo
• Boundary Conditions:
Anvil is fixed, helmet outer liner and foam liner and Head are in contact, impact
velocity of 7.5m/s
PLA can be extracted as soon as meshing and BC are finalized
22. References
22
• F. M. Shuaeib, A. M. S. Hamouda, R. S. Radin Umar, M. M. Hamdan, and M. S. J. Hashmi, “Motorcycle helmet - Part I.
Biomechanics and computational issues,” J. Mater. Process. Technol., vol. 123, no. 3, pp. 406–421, 2002.
• B. Liu, R. Ivers, R. Norton, S. Boufous, S. Blows, S.K. Lo, Helmets for preventing injury in motorcycle riders, 2008
• M. C. Tsai and D. Hemenway, “Effect of the mandatory helmet law in Taiwan,” Inj Prev, vol. 5, no. 4, pp. 290–291, 1999.
• Ouellet, J.V, Thom,D. R.,Smith, T. and Hurt Jr., H. H., 1986.,"Helmets and Neck Injuries in Fatal Crashes”
• E. A. Luce, T. D. Tubb, and A. Moore, “Review of 1,000 major facial fractures and associated injuries.,” Plast Reconstr
Surg, vol. 63, no. 1, pp. 26–30, 1979.
• P. K. Pinnoji, P. Mahajan, N. Bourdet, C. Deck, and R. Willinger, “Impact dynamics of metal foam shells for motorcycle
helmets: Experiments & numerical modeling,” Int. J. Impact Eng., vol. 37, no. 3, pp. 274–284, 2010.
• V. Kostopoulos, Y. . Markopoulos, G. Giannopoulos, and D. . Vlachos, “Finite element analysis of impact damage
response of composite motorcycle safety helmets,” Compos. Part B Eng., vol. 33, no. 2, pp. 99–107, 2002.
• R. M. Coelho, R. J. Alves de Sousa, F. A. O. Fernandes, and F. Teixeira-Dias, “New composite liners for energy absorption
purposes,” Mater. Des., vol. 43, pp. 384–392, 2013.
• Snell Foundation, 'Philosophy and Concept of Helmet Testing’, 2015. Available: http://www.smf.org/testing
• Vaitkus,S. Laukaitis,A. Gnipas, I. Kersulis, V. and Vejelis, S. “Experimental Structure and Deformation Mechanisms of
Expanded Polystyrene (EPS) Slabs” ,Materials Science, 2006
• Cui, L., Forero Rueda, M. A., & Gilrist, M. D. (2009). Optimisation of energy absorbing liner for equestrian helmets. Part
II: Functionally graded foam liner. Materials and Design, 30(9), 3414–3419.
http://doi.org/10.1016/j.matdes.2009.03.044
23. Acknowledgements
23
We would like to thank:
•Mr. Bahaa Aboulkhoudoud for his assistance in drawing the head
form according to standards
•The AUB Engineering Workshop staff particularly Joseph Zoulikian
for helping manufacture the head form by CNC Machining
•The Department of Mechanical Engineering at AUB