Aircraft Structures Stress Analysis & Simulation Engineer

Cyient; Hyderabad; On-site; INR 1,200,000 - 2,400,000; Full time

Job summary

Cyient in Hyderabad, India, is seeking an Analysis Engineer for aerostructure stress analysis, focusing on composite and metallic structures and FEM methods. The role demands extensive experience with Nastran/Patran, Hypermesh and Simcenter 3D, and the ability to work independently to deliver robust stress solutions.

The candidate should have 5–15 years in aerostructure analysis, with minimum 5 years in composite analysis, and familiarity with wingbox, load interfaces and fastener strengths.

Qualifications

• 5-15 years experience in aerostructure analysis, including at least 5 years in composite analysis.
• Experience with both composite and metallic design solutions and FEM methods.
• Knowledge of wingbox, load interfaces, and fastener/joint strength.

Responsibilities

• Perform stress analysis of aerostructure components using Hypermesh and MSC Nastran/Patran.
• Assess composite stress and familiarity with eVTOL/AAM contexts is advantageous.
• Prepare stress documentation and reports; support technical reviews and gate reviews.

Skills

Aerostructure analysis

Composite analysis

FEM methods

FEM tools

Independent working

Tools

Hypermesh

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

Roles and Responsibilities

Execute engineering duties such as Stress Analysis of Mechanical components of Aero Structure, using Hypermesh, MSC Nastran/Patran. Knowledge of composite stress is mandatory. Experience on eVTOL and AAM is an advantage