Chamara Abeykoon Email & Phone Number

Munich, Bavaria, Germany

Ankara, Turkey

Duties and Responsibilities:• Conducted classical structural analysis of aircraft structures using HSB and ESDU methods to ensure performance and safety.• Developed finite element models with HyperWorks and MSC Patran for precise structural simulations.• Performed linear and nonlinear finite element analysis with MSC Nastran and OptiStruct to assess structural behaviour.• Generated stress analysis reports to document findings and suggest design improvements.• Communicated design changes to leadership and the team to align with project objectives.• Participated in assembly and component testing to validate structural integrity.Projects:• Hürjet – Supersonic Training and Light Fighter Aircraft – Centre Fuselage, Landing Gear Fittings (Metallic and Composites)Accomplishments:• Achieved remarkably stringent weight margins through systematic design modifications and advanced non-linear analysis techniques.

Moratuwa, Western, Sri Lanka

Conducted lectures under the following topics to final year students of the department of mechanical engineering specialized in aeronautical engineering. • Aircraft Structural Design • Mechanics of Composites

Negombo, Western, Sri Lanka

Duties and Responsibilities:• Led a design and stress engineering team through complex challenges, ensuring project objectives were achieved.• Developed proprietary stress analysis tools, enhancing engineering analysis efficiency and accuracy and conducted comprehensive training sessions.• Designed aircraft repairs and modifications, prioritising safety and compliance with EASA and FAA regulations.• Checked and approved structural substantiation reports and certification documents for repairs and modifications, ensuring regulatory compliance.Accomplishments:• Spearheaded the development of a comprehensive suite of stress analysis tools and initiated a structured stress analysis training program. These initiatives standardised the structural substantiation process, significantly enhancing the quality of deliverables while optimising time utilisation.• Demonstrated exceptional performance and leadership qualities, resulting in a rapid promotion from design engineer to senior lead engineer. This progression underscored consistent excellence and notable contributions to project success within a short timeframe.

Optimization of current external fixator models with composite materials.• Identified the drawbacks in existing external fixator designs.• Selection of the composite materials to improve the designs.• Tailored the composite materials to optimize the stiffness and the weight of external fixators using the finite element method.• Conducted mechanical tests to validate the improved designs and finite element models.

Sri Lanka

Duties and Responsibilities:• Conducted comprehensive static, fatigue and damage tolerance analyses on aircraft structures using classical engineering principles and advanced finite element methods.• Produced detailed structural substantiation and certification reports to ensure compliance with EASA and FAA regulations.• Refined analysis methodologies to optimise accuracy and efficiency, drawing insights from industry standards.• Developed intricate finite element models to simulate aircraft structures under various operational conditions.• Provided technical guidance and conducted tailored training sessions on complex topics such as composite structures.• Played a pivotal role in project management, ensuring high-quality deliverables and providing dynamic technical leadership.• Established effective communication channels with stakeholders to ensure alignment on technical specifications and milestones.Projects:• Stress Analysis Tools Development (Metallic and Composite)• Aerion AS2 - Strake at the wing leading edge (Composites)• Airbus A350- MRB Support for Leading Edge Slat (Composite)• Comlux Slice of Life - Interior ceiling and sidewall assemblies (Composites)• Bombardier Global 7000/8000 - Upper wing skin and skin joints• Airbus A220-100/300 (Bombardier C Series) – Fuselage Frames, Door Surrounds, Bulkheads • Bombardier Learjet 85 – Rear Fuselage, Empennage, Fuel Pump AssemblyAccomplishments:• Secured a half scholarship and received full paid leave to pursue the MSc program at Imperial College London in 2015, enhancing knowledge and skills in aerospace engineering.• Availed opportunities to undergo specialised training and gain valuable work experience at esteemed facilities, including LMI in the USA and SONACA in Belgium, further expanding expertise and insights in stress engineering practices.

Sri Lanka

Duties and Responsibilities:• Implemented test procedures and methods to qualify restraint strap assemblies for compliance and performance.• Prepared comprehensive qualification test reports, meticulously evaluating test results and documenting findings for analysis and future reference.Projects:• ETSO C172 Aircraft Restraint Straps Certification Project.Accomplishments:• Earned selection to the R&D team by the engineering manager, who recognised outstanding technical skills and potential for contribution to innovative projects.

Master Of Science (Msc), Composites: The Science, Technology And Engineering Application Of Advanced Composites, Distinction

Related Modules: Manufacturing Science, Composite systems, Mechanical Testing, Stress Analysis, Fracture, Analysis of Laminated.

Bachelor Of Engineering (Beng), Aerospace Engineering, First Class

Related Modules: Aerospace Structures and Dynamics (A+), Aerospace Structures & Materials (A), Aerospace Engineering Design and Materials.