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    Occupant Motion and Injury Risk Analysis

    In Rollover Accident

    FHWA / NHTSA National Crash Analysis CenterThe George Washington University Virginia Campus

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    OUTLINE

    Study Purpose

    Modeling

    Input Data and Parameters

    Roof Crush

    Vehicle motion

    Results

    Conclusion

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Study Purpose

    Study relationships to injury risk to belted occupants during

    rollover.

    Driver kinematics and physical measures are predicted by

    MADYMO, an occupant modeling package, for a roll event (2.5

    rolls).

    Vehicle motion is pre-specified.

    MADYMO calculates accelerations and loads on the dummy, so

    that injury risk can be estimated.

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Parameters of the Study

    Passenger or driver side leading roll

    Shape of roof crush: No Deformation ( O ) (Baseline)

    Roof Crush In ( M )

    Roof Crush Out ( R)

    Matchbox ( S )

    A-pillar Crush ( T ) (FMVSS 216-like)

    Extent of crush: No deformation at the first roof impact; 5 at the second

    5 at the first roof impact; 10 at the second

    Side window breaking time follows first impact

    Upper interior compliant with FMVSS 201

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Roof Crush Modes

    M R

    S T

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Vehicle Motion

    Desire to model as generically as possible

    Need data on pre-roll and roll motion

    Pre-roll calculated in HVE

    Roll calculated by hand from rollover reconstructions

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Accident Reconstruction: Pre-Roll

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    NCACFHWA / NHTSA / National Crash Analysis CenterThe George Washington University

    Accident Reconstruction: Roll

    4 Rolls, Passenger Side Leading

    NOTE: For the study, only 2.5 rolls are considered.

    Airborne

    Wheel Contact

    CG Trajectory

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Ballistic For Rollover Reconstruction

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Trajectory from Pre-Roll (HVE) and Reconstruction

    Point of

    Roll

    HVE

    Data Reconstruction Data

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Simulation Matrix: 18 Cases; 2.5 rolls each

    Roll 2

    10 in

    Roll 1

    5 in

    CRU

    SH2

    Roll 2

    5 in

    Roll 1

    0 in

    CRUSH1

    TSRMOTSRMO

    Driver Leading SidePassenger Leading Side

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Results

    MADYMO allows relevant output from the dummy to

    evaluate the injury risk.

    Injury risk is calculated separately for each roll..

    Output data is normalized to the baseline (no crush) or tothe Injury Assessment Reference Values (IARV).

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Data Collected on the Dummy

    Head Acceleration,

    Velocity and

    Displacement

    Neck LoadsThorax Acceleration

    and Displacement

    Chest Deflection

    Pelvis Accelerationand Displacement

    Lap BeltLoads

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Matrix of Videos

    Roll 2

    10 in

    Roll 1

    5 in

    CRUSH2

    Roll 2

    5 in

    Roll 1

    0 in

    CRUSH1

    TSRMOTSRMO

    Driver Leading SidePassenger Leading Side

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Results

    Occupant kinematics are greatly affected by vehicle pre-

    roll and roll kinematics.

    In passenger side leading rolls, there appears to be a higher

    risk of partial ejection and ground contact.

    In driver side leading rolls, head velocity relative to thevehicle interior is significant contact related injury risk

    may be higher.

    Primary restraint is maintained by the lap belt.

    Injury metrics are being evaluated

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Limit of the study

    No contact dummy/ground

    Roll trajectory is not accurate enough to enable groundcontact at this stage.

    The model is not validated: results can only be comparedto baseline test run with the same model.

    Roof deformation is prescribed not predicted dynamically

    in real-time

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Outline

    Validation of FMVSS 216 test using LS-DYNA

    Validation of FMVSS 216 related research test with LS-

    DYNA

    Direct comparison of the standard and research tests to

    find critical orientations for the roof performance

    Conduct vehicle drop tests Validating model to all tests

    Utilize model to investigate roof behavior and relationship

    to injury risk

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    FMVSS 216 Update Research

    FMVSS 216 is a relatively old standard and is approaching

    revision.

    Vehicles may now be optimized to the standard using

    detailed computer modeling.

    Change in rotation configuration of loading device is a key

    investigative issue because: In reality vehicles, such as light trucks, can contact the ground at

    higher roll and pitch angles.

    Vehicle components (pillars, doors, roof, etc) in wider angle

    contacts may reduce ability to crush and induce bending modes.

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    FMVSS 216 Test Specifications

    216 Tests Original Updated ProtocolTest Type Static Static

    Dimensions of Loading Device (in) 30*72 30*72

    Roll Angle (deg) 25 45

    Pitch Angle (deg) 5 10

    Velocity of Loading Device (in/sec) 0.5 0.5Maximum Amount of Load (N) 60,000 60,000

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NHTSA 216 Research Tests

    25-5 config before and after test 45-10 config before and after test

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NHTSA Tests

    FMVSS 216 test w/

    25o roll & 5o pitch

    FMVSS 216 test w/

    45o roll & 10o pitch

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NHTSA Test Results

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Replicate Research Tests by finite element modeling

    Finite element model of S-10 pick up truck

    Finite element model is created to simulate roof crush for

    any scenario of impact.

    Complex finite element calculations can be solved very

    fast by running on super computers.

    FMVSS 216 tests are used as validation points.

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Finite Element Modeling of S-10 Pickup Truck

    A 4x4 Matrix can be created to describe

    the effect of rotation change:

    W/O Windshield

    W/ Windshield

    45-1025-5Test Type

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Finite Element Modeling of the S-10 Pickup Truck

    216 test with 25-5configuration.

    Without glass

    Simulation period: 0.37 sec

    Contact Velocity: 0.5

    in/sec (12.7 m/sec)

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Finite Element Modeling of the S-10 Pickup Truck

    216 test with 45-10

    configuration

    Without glass

    Simulation period: 0.37 sec

    Contact Velocity: 0.5 in/sec(12.7 m/sec)

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Finite Element Modeling of the S-10 Pickup Truck

    216 test with 45-10

    configuration

    With glass

    Simulation period: 0.37 sec

    Contact Velocity: 0.5 in/sec(12.7 m/sec)

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Multiple drop tests of Chevrolet S-10 on roof structure Simulate roof crush specifications of FMVSS 216 in dynamic drop

    Monitor impact forces with load cell plate

    Monitor timing, extent, and rate of intrusion relative to occupant

    compartment

    Monitor vehicle accelerations

    Investigate contributions of roof structure and window glass

    Instrumentation on S-10 focused on model validation Accelerometers for vehicle structural validation and effect on occupant

    interaction

    Load cell plate for vehicle structural validation String pots for structural validation and intrusion measurements

    NCAC Research Tests for Roof Crush

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Research Tests for Roof Crush

    25oFront View 5o Side View

    Drop Height = 6 (152mm)

    String Pots

    Roof Intrusion

    Accelerometers

    (Linear)

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    10 (254 mm)

    72 (1829 mm)

    30(762mm)

    Point of first contact with roof

    (approximate corner of A-pillar)

    15(127mm)

    12 Load Cells

    10 x 10

    NCAC Research Tests for Roof Crush

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Simulate drop test:

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test

    1st Impact

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test - 1st Impact

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test - 1st Impact

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test

    2nd Impact

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test - 1st Impact

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test Results

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test Results

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    NCAC Drop Test Results

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Utilize Various Test Data in Occupant Model

    Roll angles modified so that impact occurs at 25 or 45

    degrees of roll

    Pitch angles modified so that impact occurs at 5 or 10degrees of pitch

    The crush direction is on the normal to the impact (25/5

    deg or 45/10 deg) to correspond with test data loading

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Matrix of Videos

    45 / 10

    deg

    25 / 5

    degRoll and

    Pitch

    Angles

    at

    Impact

    FOIL

    Drop Test5 100 50 0

    Crush extend at first and second

    impactPassenger Side

    Leading Rolloverwith A-pillar

    crush (T mode)

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    NCACFHWA / NHTSA / National Crash Analysis Center

    The George Washington University

    Next Step Toward Evaluation:

    Validate computer model to four tests

    Investigate influence of the windshield

    Run simulations for more additional configurations withdifferent angles

    Use different materials for vehicle components (pillars,headers, etc) in order to study effect on roof crush

    resistance Integrate detailed roof performance with occupant model

    for full injury risk assessment.

    Utilize computer models to assess countermeasures andbenefits