Stress Analysis Engineer
Netherlands
On-Site
Contract
Stress Analysis Engineer
Location: Bristol
Duration: 12 Months
Start Date: ASAP
A client based in Bristol is looking for an Stress Engineer working on Primary and Secondary sectors. This will be for an initial 12 month contract.
Job Description:
• Analysis of Metallic & Composite structural components.
• Work with a team responsible for the review and analysis of aircraft structural modifications to show compliance to FAR/CAR etc. regulations.
• Development of Global Finite Element Model (GFEM) for loads.
• Development of DFEM for sizing parts having complex configuration.
• Development of Analysis templates using classical methods.
• Review technical presentations, interpret the results and present the same to Customer during PDR & CDR gates.
• Responsible for ensuring 100% quality and on-time delivery
• Conduct project review meetings to share the lessons learned and best practices to the team to improve quality
• Responsible for process improvements by developing Automation tools
• Work on complex CAE problems to assist product development
• Perform Design Modifications as per need and validating the same with FEA
Must have skills:
• Expertise in handling various structural analysis tools preferably MSC Nastran/Patran, HyperMesh etc.
• 2D & 3D Finite Element modeling of simple, moderate and complex components (Plate, Hexahedral & tetrahedral elements) using MSC Nastran/Patran or HyperMesh
• Linear and non-linear static stress analysis (Geometric, Material and contact Linearity) using MSC Nastran/Patran
• Ability to interpret, modify MSC Nastran command statements in bulk data file and re-run analysis; Ability to de-bug FEA errors; perform batch runs for multiple BDFs etc.
• Hand Calculations, able to propose methods for structural failure modes
• Review and understand Strength, stability and Durability requirements of structural components
• Able to perform F&DT analysis.
• Understand/modify TCL macros; Develop MS Excel templates and comprehend VBA in developing automation
• Should able to propose methodology and strategy for complex metallic and Composites build/update of FE Models in Patran/HyperMesh.
• Methods/Process/Procedures similar to Airbus, Boeing, Bombardier and or any defense programmes.
• Experience in scripting using Mathcad, VB,TCL/Tk, Python is an added advantage
• Basic Knowledge of CAD tools is an added advantage
• Experience in Product development life cycle of aircraft components from Design concept, Analysis to Manufacturing
• PLM tools like Teamcenter, Windchill etc.,
• Experience in the use of ISAMI, Airbus tools.
• Stress Signatory experience will be added advantage.
#LI-MJ1
Location: Bristol
Duration: 12 Months
Start Date: ASAP
A client based in Bristol is looking for an Stress Engineer working on Primary and Secondary sectors. This will be for an initial 12 month contract.
Job Description:
• Analysis of Metallic & Composite structural components.
• Work with a team responsible for the review and analysis of aircraft structural modifications to show compliance to FAR/CAR etc. regulations.
• Development of Global Finite Element Model (GFEM) for loads.
• Development of DFEM for sizing parts having complex configuration.
• Development of Analysis templates using classical methods.
• Review technical presentations, interpret the results and present the same to Customer during PDR & CDR gates.
• Responsible for ensuring 100% quality and on-time delivery
• Conduct project review meetings to share the lessons learned and best practices to the team to improve quality
• Responsible for process improvements by developing Automation tools
• Work on complex CAE problems to assist product development
• Perform Design Modifications as per need and validating the same with FEA
Must have skills:
• Expertise in handling various structural analysis tools preferably MSC Nastran/Patran, HyperMesh etc.
• 2D & 3D Finite Element modeling of simple, moderate and complex components (Plate, Hexahedral & tetrahedral elements) using MSC Nastran/Patran or HyperMesh
• Linear and non-linear static stress analysis (Geometric, Material and contact Linearity) using MSC Nastran/Patran
• Ability to interpret, modify MSC Nastran command statements in bulk data file and re-run analysis; Ability to de-bug FEA errors; perform batch runs for multiple BDFs etc.
• Hand Calculations, able to propose methods for structural failure modes
• Review and understand Strength, stability and Durability requirements of structural components
• Able to perform F&DT analysis.
• Understand/modify TCL macros; Develop MS Excel templates and comprehend VBA in developing automation
• Should able to propose methodology and strategy for complex metallic and Composites build/update of FE Models in Patran/HyperMesh.
• Methods/Process/Procedures similar to Airbus, Boeing, Bombardier and or any defense programmes.
• Experience in scripting using Mathcad, VB,TCL/Tk, Python is an added advantage
• Basic Knowledge of CAD tools is an added advantage
• Experience in Product development life cycle of aircraft components from Design concept, Analysis to Manufacturing
• PLM tools like Teamcenter, Windchill etc.,
• Experience in the use of ISAMI, Airbus tools.
• Stress Signatory experience will be added advantage.
#LI-MJ1
19003UA2
| Engineering: | Mechanical |
