History and Values
Clients

Software Development: Pneumatics
Aeronautic Regulation

Approach
Training and Tutoring

Computer Aided Design (CAD)
Computer Aided Engineering (CAE) & Finite Element Method (FEM)
Linear and non-Linear Static Analysis
Fatigue and Durability
Dynamic Response
Dynamic non-Linear Analysis
Multibody Analysis
Laminate and Composite
Thermal Analysis
Special Analysis

Basic Physical Flow Modeling
Aerogasdynamics
Supersonic/Hypersonic Aerodynamics
Thermo Fluid Dynamics
Turbulence Modeling
Moldflow Analysis
Vibro Acustics
Special Analyses

Static Aeroelastic Analysis
Flutter Analysis
Dynamic Aeroelastic Response
Sensitivity and Optimization

ULM SG STORM - Structural Analysis - Part I: CAD/FEM Models
ULM SG STORM - Structural Analysis - Part II: Stress Analysis Results
ULM SG RALLY 105 S - Structural Analysis - Part I: CAD/FEM Models
ULM SG RALLY 105 S - Structural Analysis - Part II: Results, Positive 6.6 G
ULM SG RALLY 105 S - Structural Analysis - Part III: Results, Negative 3.3 G
ULM SG RALLY 105 S - Aerodynamic Analysis - Part I: Numerical Visualization
ULM SG RALLY 105 S - Aerodynamic Analysis - Part II:Technical Characteristics
ATR Flight Vehicle- CAD/FEM Models - Unsponsored

Automotive General Presentation - Overview
Irisbus Bus Model 380 - Structural Analysis - Part I: CAD/FEM Models
Irisbus Bus Model 380 - Structural Analysis - Part II: Stress Analysis Results
Irisbus Bus Model 3491 - Structural Analysis - Part I/II: CAD/FEM/Stress Analysis Results
Irisbus Bus Model 391 CNG - Structural Analysis - Part I/II: CAD/FEM Models/Stress Analysis Results
OCAP - Contact Problem in a Spherical Node - Stress Analysis

Crank - Connecting Rod IF V1312 - Structural Analysis - Part I/II: CAD/FEM Models/Stress Analysis Results

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