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Aero_Stress_Fatigue and Damage Tolerance Lead Cyient

10.0 - 15.0 years

10 - 15 Lacs

Hyderabad

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Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards (e.g., FAA, EASA). Utilize tools like NASGRO , DARWIN , or other proprietary applications for crack growth and fracture mechanics analysis. Conduct life prediction assessments under static and dynamic loading conditions, including variable amplitude loading. Support aircraft certification programs by providing substantiation reports and analysis documentation. Work closely with design, stress, materials, and manufacturing teams to define inspection intervals and structural integrity requirements. Interpret test data and validate analytical models against physical test results. Develop and review fatigue test plans and evaluate test outcomes. Document assumptions, methodologies, and results in clear, traceable technical reports. Bachelor’s or Master’s degree in Mechanical, Aerospace, or Structural Engineering. 7 to 15 years of experience in fatigue and damage tolerance analysis. Hands-on experience with at least one of the following tools: NASGRO , DARWIN , or equivalent. Experience on Stress Concentration evaluation fro Joints and Notches Solid understanding of fracture mechanics , crack growth behavior , and fatigue life prediction methodologies. Ability to use FE tools like HM and Patran for Extraction of Loads/stress for FDT analysis. Familiarity with aerospace materials, especially metallic alloys used in aircraft structures. Experience working in a regulated environment with exposure to FAA/EASA certification processes . Strong analytical, problem-solving, and documentation skills. Excellent communication skills and ability to work collaboratively in a multidisciplinary team.

Posted 12 hours ago

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Aircraft Structures Stress Analysis & Simulation Engineer Cyient

10 - 15 years

12 - 17 Lacs

Hyderabad

Work from Office

Minimum 5-15 years experience in aerostructure analysis, with minimum of 3 years of experience in composite analysis. Excellent knowledge of Aircraft Primary and Secondary structureal components. Hands-on experience with relevant tools (ISAMI, NASGRO, MSC Nastran/Patran and Altair Hypermesh). Experience on Simcenter 3D is an advantage. Knowledge on CATIA is desirable Strong experience in Static Strength, Fatigue & Damage Tolerance Analysis of aircraft primary structures A strong theoretical and practical foothold on analyses of metallic and composite structures Domain-wide experience from initial sizing to aftermarket services A well-balanced expertise including a sound understanding of basic structural concepts, hand calculations Knowledge of concessions and MRB

Posted 3 months ago

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