AeroStructures Stress Lead

Cyient; Hyderabad; Sur place; INR 2 000 000 - 3 200 000; Plein temps

Résumé du poste

Cyient Limited is seeking an experienced Structural/Aeroelastic analyst in Hyderabad to lead stress analysis and aerostructure design efforts. You will apply FEM techniques and classical methods to wings, fuselage, and other components, ensuring regulatory compliance and optimal weight.

Collaboration with design and systems teams is essential. The role requires strong analytical skills, good communication, and the ability to manage multiple projects in a fast-paced aerospace environment.

Qualifications

• 7+ years of experience in stress analysis and design of aerostructures.
• In-depth knowledge of structural analysis methods, including FEM and hand calculations.
• Experience with FAA/EASA regulatory standards and certifications.

Responsabilités

• Perform detailed static analysis on aerostructures such as wings, fuselage, landing gear, and components.
• Use FEA tools like NASTRAN, PATRAN, and HyperMesh to model structural performance under various loads.
• Ensure compliance with FAA, EASA, and military regulations and participate in design reviews.
• Develop and validate analytical methods using Excel and macros.
• Lead technical reports and communicate results to stakeholders and customers.
• Collaborate with cross-functional teams to optimize weight and manufacturability.
• Mentor and guide junior engineers and analysts.
• Identify structural risks and provide mitigation strategies.
• Support customer discussions and present on structural design and analysis.
• Explore design alternatives to improve performance.

Connaissances

Stress analysis

FEM

Material knowledge

Technical writing

Cross-functional teamwork

Formation

Bachelor's degree in Aerospace/Mechanical

Master's degree in Aerospace/Mechanical

Outils

NASTRAN

PATRAN

HyperMesh

Excel Macros

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