Project Card 05

Finite Element Simulation of Thoracic Compression and Injury Criteria


Project Pathway

🟦 Numerical / Computational Modeling (FEM)


1. Background & Motivation

Thoracic injuries are a leading cause of morbidity and mortality in automotive crashes, falls, and blunt impact accidents. The thorax exhibits a complex biomechanical response due to its composite structure, including ribs, sternum, spine, and internal organs. Injury mechanisms range from rib fractures to lung contusions and cardiovascular injuries.

In trauma biomechanics, thoracic injury risk is commonly assessed using global kinematic and deformation-based injury criteria, such as chest acceleration, chest compression, and the Viscous Criterion (VC). Finite element (FE) modeling provides a valuable tool for studying thoracic response under controlled loading conditions and for comparing the behavior of different injury criteria.

This project focuses on developing and using a simplified FE model of the thorax to investigate thoracic compression mechanisms and evaluate commonly used thoracic injury criteria.


2. Core Biomechanical Question

How do thoracic compression characteristics and loading conditions influence thoracic injury criteria predicted by a simplified finite element model?


3. Injury Mechanisms & Relevant Injury Criteria

The project should address the following biomechanical aspects:

  • Thoracic injury mechanisms:
    • Chest wall compression
    • Rib cage deformation
    • Rate-dependent thoracic response
  • Frontal blunt loading scenarios

Relevant thoracic injury metrics may include:

  • Chest compression (deflection-based criteria)
  • Chest acceleration
  • Viscous Criterion (VC)
  • Combined thoracic indices (conceptual discussion)

Students must justify the selection of injury criteria and explain their biomechanical significance and limitations.


4. Modeling / Analysis Approach

This is a numerical FEM-based project using a simplified thoracic model.

The student is expected to:

  • Develop or adapt a simplified FE representation of the thorax
  • Model key structural components (rib cage, sternum, spine) at a conceptual level
  • Apply frontal compression or impact loading representative of thoracic trauma
  • Compute and interpret thoracic injury metrics

High anatomical fidelity is not required. The emphasis is on mechanisms, trends, and injury metric interpretation.


5. Technical Specification (Core Section)

The project must include a clear and structured description of:

a) Geometry and Model Structure

  • Simplified thoracic geometry
  • Representation of ribs and sternum
  • Justification of geometric simplifications

b) Material Modeling

  • Material assumptions for bony and soft tissues
  • Rate-dependence or damping (if considered)
  • Rationale for parameter selection

c) Boundary Conditions and Loading

  • Loading configuration (e.g., rigid impactor, distributed compression)
  • Loading rate or velocity
  • Constraints and contacts

d) Output Quantities

  • Chest deflection and compression
  • Chest acceleration
  • Computation of VC and other injury metrics
  • Post-processing workflow

6. Parametric / Sensitivity Study

A limited parametric study is required, such as:

  • Variation of loading rate or impact velocity
  • Variation of thoracic stiffness parameters
  • Comparison between different injury criteria responses

The goal is to identify relative trends and sensitivities, not absolute injury thresholds.


7. Validation Strategy & Limitations

The project must explicitly discuss:

  • Qualitative or quantitative comparison with published thoracic impact experiments
  • Sensitivity of injury metrics to modeling assumptions
  • Limitations related to:
    • simplified thoracic anatomy,
    • absence of internal organ modeling,
    • lack of experimental validation

Students must clearly state which conclusions are supported by the model.


8. Feasibility & Computational Considerations

The project must address:

  • Software used (e.g., Abaqus/Explicit, LS-DYNA)
  • Computational cost and runtime
  • Mesh density and timestep considerations
  • Numerical stability and contact handling

Models requiring excessive computational resources are discouraged.


9. Expected Outcomes

By the end of the project, the student should deliver:

  • A simplified FE thoracic compression model
  • Computed thoracic injury metrics for selected loading scenarios
  • Sensitivity analysis results
  • A critical interpretation of thoracic injury predictions

The outcome should demonstrate numerical competence and biomechanical insight.


10. Deliverables

  1. Final Report (20-25 pages, excluding appendices)
  2. Model description and representative figures
  3. Injury metric plots and tables
  4. Oral presentation (15-20 minutes)

Optional appendices:

  • Input files
  • Post-processing scripts
  • Additional simulation cases

11. Project-Specific Grading Rubric

CriterionDescriptionWeight
Problem formulation & relevanceClear definition of thoracic injury scenario10%
Injury mechanism understandingCorrect interpretation of thoracic biomechanics15%
Injury metric selection & justificationAppropriate and critical use of thoracic criteria10%
FEM model formulationQuality of geometry, materials, BCs, and assumptions20%
Parametric / sensitivity analysisInsightful exploration of trends and criteria comparison15%
Validation & limitationsRealistic discussion of model credibility15%
Technical clarity & professionalismQuality of documentation and figures15%
Total100%

12. Project Scope Agreement

By choosing this project, the student agrees to:

  • Emphasize injury mechanism interpretation over model complexity
  • Clearly document assumptions and limitations
  • Avoid overinterpretation of simplified injury predictions

Note:
Thoracic injury criteria are context-dependent; understanding their assumptions is as important as computing their values.

Seyed Sadjad Abedi-Shahri
Seyed Sadjad Abedi-Shahri
Assistant Professor of Biomedical Engineering

My research interests include Numerical Methods in Biomechanics, Scientific Computation, and Computational Geometry.