Polyvios Gregoriades - Part time Stress Engineer
Experience
Part time Stress Engineer
Manna Drones Ltd
- Supported the development of a new composite air-frame using ANSYS finite element analysis
- Supported the team in various stress engineering activities related to sizing and optimizing metallic components
Senior Stress Engineer – Airbus A220
SPIRIT Aerosystems
- Fixed leading edge (FLE) major in service problem (MISP) solution using FEM (MSC Patran/Nastran, Altair Hypermesh, SAMCEF, Simcenter-3D) and hand calculations
- Worked towards an acceptable fatigue and damage (durability) solution and redesign of the FLE
Senior Stress Engineer – Mitsubishi HI-H3 Launcher
RUAG Space
- Sizing of the umbilical door situated at the payload fairing (PLF) using FEM (MSC Patran/Nastran, Altair Hypermesh/Hyperview) and hand calculations
- Worked towards critical design review report
Senior Stress Engineer – A321 XLR
AIRBUS Deutschland
- Generated detailed finite element models integrated into A321 XLR single slotted flap model using Hypermesh/Hyperview
- Performed analysis (MSC Nastran) on a subset of loadcases to support preliminary design sizing
Senior Stress Engineer – A350 XWB-900
AIRBUS Deutschland
- Static stress assessment of Jack Catcher Brackets supporting actuators of Spoiler No. 4 in case of actuator pin failure using 3D finite element modelling (Hypermesh/Hyperview/MSC Nastran) and HSB Stress Manual
- Achieved significant weight reduction from previous design using Altair OptiStruct
Senior Stress Engineer – A320 Ultimate
AIRBUS Germany
- Preliminary sizing of hinged flap design concept for the future A320 Ultimate wing through hand calculations (HSB Stress Manual) and finite element analysis (Hypermesh/Hyperview, MSC Nastran)
- Performed weight optimization using Altair OptiStruct
- Met weight and stiffness constraints
Senior Engineer
The Cyprus Institute
- Provided fundamental aerodynamics analysis
- Performed structural analysis
- Conducted finite element analysis for the development of UAVs at the Unmanned Systems Research Laboratory
Senior Stress Engineer – Embraer 175E2
SONACA Sprl
- Sized Embraer 175 flaps using in-house finite element analysis tools (SONIA-SAMCEF) and hand calculations
- Conducted fatigue and damage tolerance analysis on lugs (NASGRO)
Senior Stress Engineer – ATLAS V 5.4m PLF
RUAG Space
- Sized air-conditioning duct of the payload fairing (PLF) using FEM (MSC Patran/Nastran, Altair Hypermesh) and hand calculations
- Worked towards critical design review report
Senior Stress Engineer – T-X Trainer Prototype
SAAB Aerostructures
- Sized engine bay components including engine inlet wall mounts, engine inlet ducts and air inlet components using hand calculations in Mathcad
- Created detailed FEM components using Altair Hypermesh and MSC Nastran
- Supported early completion of the T-X prototype to assist Saab-Boeing bid for U.S. Air Force Trainer-X competition
Senior Stress Engineer – Airbus A350 XWB-1000
SAAB Aerostructures
- Supported the Flap Support Structure team for sizing composite fairings of the A350
- Generated FEM (MSC Patran, Altair Hypermesh) and performed stiffness and strength calculations (MSC Nastran, Airbus ISAMI 8.1) along with hand calculations
- Worked towards C-scheme approval
Senior Stress Engineer – Clean Sky Smart Fixed Wing
ASCO Industries
- Sized Krueger flaps consisting of metallic components and composite panel using classical hand calculations and finite element analysis (MSC Patran/Nastran)
- Completed C-scheme approval signed off by Airbus Deutschland
- Improved and further developed ASCO’s composite analysis tools
Stress Engineer – A350XWB-900 Composite Wingtip-Winglet
AIRBUS UK
- Sized wingtip to winglet joint composite and metallic structural components to achieve B-Scheme sign-off by Airbus using classical hand calculations, Airbus metallic and composite methods and finite element analysis
- Advised design team throughout sizing iterations to achieve optimum structure
Stress Engineer – Airbus A380
AIRBUS Deutschland GmbH
- Performed post-buckling analysis of A380 composite flaps and test panels using non-linear finite elements (ABAQUS) and hand calculations
- Authored structural repair manual for midboard and outboard flaps
Consulting Engineer
Upperstage Engineering Ltd
- Provided engineering consultancy services for industrial and research projects
- Conducted stress and finite element analysis (ANSYS) of deep-sea autonomous underwater vehicle (European funded project)
- Performed impact analysis on motorway guardrails using LS-DYNA 3D
Stress Engineer – Ariane 5 Launcher
ASTRIUM GmbH
- Conducted ESC-A line interface analysis using hand calculations and in-house software
- Performed structural verification and dynamic and sine response analysis for SYLDA 5 internal payload carrying structure to permit double satellite launch configurations
- Executed structural finite element analysis for test verification and dynamic analysis of the Cone-3936 payload carrier structure
- Analyzed ceramic-composite elevon for the NASA-X33 reusable launch vehicle
Professional Engineer
British Aerospace - AIRBUS Ltd
- Developed knowledge based engineering solutions for sizing metallic and composite top and bottom wing skins with stringers for multiple stringer options
- Performed structural optimization using MSC/NASTRAN solution 200 on an A321-Hybrid wing model (inner metallic and outer composite)
- Evaluated finite element analysis program NISA using NAFEMS and in-house evaluation problems for applicability in the composite wing programme
Operations Officer
Eurocypria Airlines Ltd
- Coordinated daily airline operations for the Ground Operations Department
- Liaised with airport authorities, catering services and flight operators
- Generated flight plans and crew rosters
- Conducted flight watch and supported abnormal operations including aircraft diversions
- Produced A320 aircraft performance charts
Industry Experience
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Experienced in Aerospace and Defense, Construction, Professional Services, and Space Exploration.
Business Area Experience
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Experienced in Product Development, Research and Development, Quality Assurance, and Operations.
Summary
Twenty six years of experience as a stress engineer in the aerospace industry with expertise in finite elements and hand calculations for lightweight metallic and composite structures. Worked in many areas of the aerospace industry, mainly in civil aircraft and space launchers.
Skills
- Excellent Knowledge Of Finite Element Analysis Packages: Msc Patran /Nastran, Altair Hypermesh / Hyperview / Optistruct, Samcef, Femap, Abaqus.
- Excellent Knowledge Of Object Oriented Programming Language: Python. Proficient In Building Engineering Analysis Applications And Multi-user Web Application Platforms.
- Very Good Knowledge Of Mathcad, Matlab, And Microsoft Excel Vba.
- Good Knowledge Of Computer-aided-design Software: Catia V5.
Languages
Education
University of Bristol
Master of Science, Aerospace Design, Manufacture and Management · Aerospace Design, Manufacture and Management · Bristol, United Kingdom
Iowa State University
Master of Science, Aerospace Engineering · Aerospace Engineering · Ames, United States
Iowa State University
Bachelor of Science, Aerospace Engineering · Aerospace Engineering · Ames, United States
Certifications & licenses
Certified Daily Coastal Yacht Skipper
American Sailing Association
Statistics
Experience
Global Experience
Expertise
Qualifications
Profile
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