05/30/2025 updated
100 % available
Aeronautical Engineer with 13+ years experience in Aircraft Structures and Automotive Design
Sundbyberg, Sweden
Worldwide
Bachelor's Degree in Aeronautical EngineeringComputer-Aided DesignAerospace EngineeringAutomotive DesignAutomotive EnginesWeldingBoundary Value ProblemChange ManagementSolidWorks (CAD)Finite Element MethodsFemapProject ManagementNastran (Computer-Aided Design Software)Product DesignStress TestingTest Planning
Aircraft Interior Structures
Expertise in designing and analyzing aircraft interior structures including galley, closet, lavatory, and curtain track components with focus on certification standards.
Finite Element Analysis
Advanced knowledge in performing static stress analysis, applying loads and boundary conditions, and validating designs through FEM techniques.
Automotive Body-in-White Design
Specialized skills in designing underbody components, managing welding joints, and implementing EBOM for automotive body structures.
CAD/CAE Software Proficiency
Extensive experience with CATIA v5/v6, FEMAP with NX NASTRAN, ENOVIA v6, Solidworks, MSC PATRAN-NASTRAN, and 3DExperience.
Certification Documentation
Preparation of detailed stress dossiers for FAA and EASA type certifications, including test plans and strength substantiation reports.
Product Development
Comprehensive approach to product development with focus on design optimization and cost-saving initiatives.
Project Management
Skills in coordinating change management, component release tracking, and cross-functional team collaboration.
Expertise in designing and analyzing aircraft interior structures including galley, closet, lavatory, and curtain track components with focus on certification standards.
Finite Element Analysis
Advanced knowledge in performing static stress analysis, applying loads and boundary conditions, and validating designs through FEM techniques.
Automotive Body-in-White Design
Specialized skills in designing underbody components, managing welding joints, and implementing EBOM for automotive body structures.
CAD/CAE Software Proficiency
Extensive experience with CATIA v5/v6, FEMAP with NX NASTRAN, ENOVIA v6, Solidworks, MSC PATRAN-NASTRAN, and 3DExperience.
Certification Documentation
Preparation of detailed stress dossiers for FAA and EASA type certifications, including test plans and strength substantiation reports.
Product Development
Comprehensive approach to product development with focus on design optimization and cost-saving initiatives.
Project Management
Skills in coordinating change management, component release tracking, and cross-functional team collaboration.
Experience
Professional experience10+ years
Freelancer since2025
Languages
EnglishFluentFrenchBasic knowledgeHindiNative speakerSwedishGood
Project history
- FEM preparation of aircraft interior group comprising of galley, closet, lavatory, curtain track, cupboard, pocket door, credenza, conference table etc.
- Application of loads, boundary conditions and performing static stress analysis
- Prepared detailed stress dossier for FAA type certification
- Performed hand calculations for validation
- Prepared static test plan for full scale monument testing
- Designed body in-white underbody components such as rear panel assembly, seat mounting brackets, spare wheel housing, floor panel, wheel arch assembly
- Collaborated with cross functional simulation teams such as crash, durability and NVH, to understand vehicle behaviour and propose alternate design solutions
- Managed vehicle level welding joints, sealant definitions in body shop and paint shop lines
- Handled body in-white EBOM, tracking component release and coordinating change management in PDM tool
- FEM preparation of A350 interior monuments from the given CAD data
- Application of loads, boundary conditions, performing static stress analysis and post processing
- Detailed stress report preparation for EASA type certification
- Performing hand calculations for validation
- Preparation of static test plan for full scale monument testing and qualification
- Test report preparation post full scale testing for EASA type certification
- Strength substantiation report preparation by similarity analysis method, to avoid physical testing as cost saving initiative