Key Responsibilities

1. Perform linear and nonlinear static stress analysis of composite structures.
2. Conduct buckling analysis of composite panels, spars, ribs, and stiffened structures.
3. Perform fatigue and durability analysis, and apply appropriate composite failure criteria
4. Perform modal analysis to determine natural frequencies, mode shapes, and modal participation

factors.
1. Support vibration, resonance, and structural dynamic assessments for Flight loads, Payload-

induced excitations, Launch, recovery, and transportation conditions
1. Contribute to flutter margin assessments and stiffness tailoring of composite structures.
2. Collaborate with aerodynamics, propulsion, and systems engineering teams to ensure structural

integrity and performance.
1. Prepare technical reports, documentation PDR, CDR & TRR
2.



Ensure compliance with aerospace industry standards (DGCA, DGAQA- MIL).
3. Mentor junior engineers and contribute to continuous improvement of analysis methodologies.

Required Skills & Competencies:
1. Expertise in Mechanics of composite materials, Classical Laminate Theory (CLT), Strength of

materials, structural dynamics & vibration
1. Proficiency in FEA tools such as: ANSYS / NASTRAN , HyperMesh
2. CAD Interface: CATIA / NX / SolidWorks
3. Dynamic Analysis: Modal solvers, frequency response tools
4. Experience interpreting mode shapes, frequency shifts, and buckling eigenvalues
5. Solid understanding of load paths and stiffness-driven design

📌 Lead Stress Engineer (Odisha)
🏢 CIEL HR
📍 Odisha