Aero Structures Stress Lead

Cyient; Hyderabad; Sur place; INR 2 500 000 - 3 800 000; Plein temps

Résumé du poste

Cyient Limited in Hyderabad seeks a senior structural analyst with 7+ years in stress analysis and aerostructure design to join a fast-paced, multidisciplinary team.

You will perform static analyses, FEM/FEA, and ensure compliance with FAA/EASA standards while collaborating with design, materials and systems teams to optimize weight, reliability and safety.

Qualifications

• 7+ years of experience in stress analysis and aerostructure design.
• In-depth knowledge of structural analysis methods including FEM, hand calculations, and failure theories.
• Proficiency with NASTRAN, PATRAN, and HyperMesh or similar FEA tools.
• Strong aerospace materials knowledge: composites, metals, and advanced alloys.
• Familiarity with aircraft systems integration.
• Solid understanding of aerospace loads and regulatory standards (FAA, EASA).
• Excellent communication and ability to manage multiple projects.
• Ability to work in a fast-paced, multidisciplinary team environment.

Responsabilités

• Perform detailed static analysis using classical hand calculations on aerostructures (wings, fuselage, landing gear, floor beams, doors).
• Utilize FEA software such as HyperMesh, NASTRAN, PATRAN to model and analyze structural performance under various loading conditions.
• Ensure compliance with FAA, EASA, and military regulations; participate in design reviews.
• Experience on Airbus and Boeing aircraft structures is an added advantage.
• Develop and validate analytical methods using Excel and Macros for predicting structural component behavior.
• Collaborate with design engineers on material selection, design changes, and manufacturing processes to optimize weight while maintaining safety.
• Lead technical reports and documentation to communicate results and compliance; prepare certification reports for PDR/CDR.
• Include mitigations and summarize Reserve factor in reports.
• Mentor junior engineers and analysts.
• Collaborate with cross-functional teams (materials, design, systems) for integrated, efficient designs.
• Identify and address structural performance risks and provide solutions to improve reliability.
• Participate in customer discussions and presentations on structural design and analysis.
• Conduct optimization studies to enhance efficiency, reduce weight, and improve manufacturability of fuselage components.

Connaissances

FEA / FEM

Hand calculations

Failure theories

NASTRAN

PATRAN

HyperMesh

Aerospace materials

Aircraft systems integration

FAA / EASA regulations

Problem solving

Technical report writing

Cross-functional teamwork

Formation

Bachelor's degree in Aerospace or Mechanical Engineering

Master's degree in related field

Outils

HyperMesh

NASTRAN

PATRAN

Description du poste

Bachelor's, Master's, in Aerospace Engineering, Mechanical Engineering, or a related field.

7+ years of experience in stress analysis and design of aerostructures, preferably in the aerospace industry.

In-depth knowledge of structural analysis methods, including finite element modeling (FEM), classical hand calculations, and failure theories.

Proficient in FEA tools such as NASTRAN/PATRAN/HM similar software.

Strong understanding of aerospace materials, including composites, metals, and advanced alloys.

Familiarity with aircraft systems and the integration of structures with other aircraft systems.

Solid understanding of aerospace loads and regulatory standards and certifications (e.g., FAA, EASA).

Strong problem-solving skills, attention to detail, and ability to manage multiple projects simultaneously.

Excellent written and verbal communication skills, including technical report writing and presentations.

Ability to work in a fast-paced, multidisciplinary team environment.

Roles and Responsibilities

• Perform detailed static analysis using classical Hand calcualtion, on aerostructures, including wings, fuselage, landing gear, Floor beam, Doors and other aircraft components.
• Utilize Finite Element Analysis (FEA) software, such as HYPERMESH, NASTRAN, PATRAN to model and analyze structural performance under various loading conditions.
• Ensure compliance with aerospace industry standards, including FAA, EASA, and military regulations, and participate in design reviews.
• Experience on Airbus and Boeing Aircraft structures is an added advantage.
• Develop and validate analytical methods using excel and Macros techniques to predict the behavior of structural components.
• Work closely with design engineers to provide input on material selection, design changes, and manufacturing processes to optimize structural performance and minimize weight while maintaining safety.
• Lead technical reports and documentation to communicate analysis results, design recommendations, and compliance to regulatory bodies and customers. Preparing the certification standard report with detailed explanations of procedures followed for analyzing a structure to support PDR and CDR.
• Include all the mitigations and summarize Reserve factor in the report
• Mentor and provide guidance to junior engineers and analysts.
• Collaborate with cross-functional teams (materials, design, systems, etc.) to ensure integrated, efficient, and safe structural designs.
• Identify and address structural performance risks, and provide solutions to improve the overall reliability and performance of aerostructures.
• Participate in customer-facing discussions and presentations related to structural design and analysis.
• Conduct optimization studies to enhance structural efficiency, reduce weight, and improve manufacturability of fuselage components. Explore design alternatives to achieve optimal performance