Aircraft Structures Stress Analysis & Simulation Engineer

Cyient; Hyderabad; On-site; INR 900,000 - 1,500,000; Full time

Job summary

Cyient seeks an experienced Analysis Engineer to support stress analysis of aerostructures in Hyderabad, India. The role covers both composite and metallic design solutions, using classical methods and finite element analysis to assess strength, stiffness, buckling, and damage tolerance.

You will prepare stress documentation and participate in technical reviews. Independent work with minimal supervision is required, along with guidance to junior engineers and collaboration across teams and with

Qualifications

• Minimum 5 years of aerostructure stress analysis experience.
• Experience in composite structures and metallic designs.
• Ability to perform FEA and interpret results.

Responsibilities

• Perform stress analysis on aerostructures using classical methods and FEM.
• Create stress documentation, provide justifications and reports.
• Support reviews with technical data and presentations.
• Work with cross-functional teams and guide other engineers.

Skills

Aerostructure analysis

Composite analysis

Finite element analysis

Stress documentation

FEM post-processing

Cross-functional collaboration

Tools

Nastran/Patran

Simcenter 3D

Job description

• 5-15 years experience in aerostructure analysis, with minimum of 5 years of experience in composite analysis.

• Thorough familiarity with primary and secondary aircraft structures and load behaviours

• An Analysis Engineer is required to support stress analysis of aerostructures. The candidate is required to be capable, flexible, and to be able to work independently to assess both composite and metallic design solutions using a variety classical stress methods and finite element analysis. Be able to conduct a variety of stress analysis on both composite and metallic structures including general strength analysis, stiffness assessments, buckling and stability strength, fastener and joint strength, standard composite strength analysis of both sandwich and thermoset composite panels, composite damage tolerance analysis of open hole strength and compression-after-impact strength. Have a good understanding of structural design (e.g. Wingbox) including understanding load and stiffness requirements, design of load interfaces such as flap and moveable surfaces and wingbox to fuselage connections Be able to perform finite element analysis using GKN recognized toolsets (such as Nastran/Patran, Simcenter 3D). Candidate should be capable of creating, modifying, and post-processing results from FEM models. Generate stress documentation including reserve factor summaries, detailed stress justifications, and certification reports Perform all activities at a level of minimal supervision and guide other engineers within the work package as required. Identify, analyse and resolve technical problems and apply/integrate solutions. Develop, execute, and verify methods plans, toolsets and approaches that are appropriate and compliant to achieve the design and programme objectives. Identify and assess technical risk and propose mitigations relevant to the workpackage within assigned programmes/projects. Be able to interpret and process design data including interfaces, dimensions, materials, parts, manufacturing process requirements, assemblies, and tolerances as part of the stress analysis of components. Deliver assigned project deliverables, documents, and reports to the required quality standards and within the assign project target milestones. Work within a team environment both locally and remotely. Support and participate in technical and customer reviews, including formal gate reviews, including the creation and preparation of technical data and presentations of a work package. Support the qualification process of products within a work package, and prepare and/or check compliance.