Thomas Godwin Email & Phone Number

Wetzikon, Zurich, Suisse

Technical Project Lead of the AW09 Helicopter Fuel System- Responsible of the design, development, integration, qualification and certification of the system- Distribution of the workload within the team with other System/Design Engineers - Liaison with supplier and external partners- Point of contact with Project, Customer Support, Production, Testing and other Engineering Teams- Presentation to the European authorities (EASA) as part of the CS.27 certification- Documentation/substantiation to ensure flight safety and provide flight clearance- Creation of Test Procedure/Report supporting the Development and the Certification- Support to the Production Line for assembly issues and equipment deviations

- Design, development, integration, qualification and certification of the system- Liaison with supplier and external partners- Point of contact with Project, Customer Support, Production, Testing and other Engineering Teams- Presentation to the European authorities (EASA) as part of the CS.27 certification- Documentation/substantiation to ensure flight safety and provide flight clearance- Creation of Test Procedure/Report supporting the Development and the Certification- Support to the Production Line for assembly issues and equipment deviations

Donauwörth

Clean Sky 2 - Racer- System and equipment technical development and qualification with dedicated partners- Modeling and performance analysis of the fuel vent/pressure refueling/feeding system- Technical documentation (Technical Note, Specification, etc.)- Point of contact with Project, Testing and other Engineering TeamsNH90 External and Internal Auxiliary Fuel Tanks:- Provide technical support for in services issues at customer level- Manage equipment technical change with suppliers- Document review/writing (Hazard Assessment, Equipment Change Proposal, Maintenance, etc.)- Supplier management

Région De Berlin, Allemagne

Aerodynamic Engineer in the Nacelle Aerodynamic department- CFD studies on the Nacelle Installation (Air Intake, Exhaust System, Thrust Reverser, Bypass-Duct).- Performance studies of a Variable Area Nozzle, studies of the 3D effects of the installed nacelle

Vernon

6-month internship, in a company designing and producing the liquid rocket engines for European launchers, as an intern in the Bearing and Seal department- Improvement of the CFD modeling of hole-pattern annular seal of space turbopump - Comparison of methods for the determination of the friction factor of such seals - Comparison of the CFD results (RANS simulations) with PhD Thesis done on the subject- Influence study of the mesh refinement - Influence study and determination of the best turbulence model for such flows- Comparison between the CFD and experimental results on the static characteristics (pressure profile, leakage massflow)- Implementation of new friction law in the 1D/2D tools developed in the company

Région De Munich, Allemagne

6-month Master’s thesis in the aerospace propulsion department of the TUM. Turbopump activities for launch vehicle and suborbital flight within the KonRAT project (TUM, German Space Center, Airbus D&S) Preliminary design of the turbine of an LOX turbopump- Literature research and reading about the turbine design- Aerodynamic preliminary design of the turbine of an LOX turbopump: main requirements on the required power needed by the pump and the low pressure drop across the turbine- Writing of a MATLAB script giving the flow deviation across the turbine and the profile of its blade (interpolation of third-degree polynom)- Meshing of the obtained profile with ICEM CFD- Steady RANS simulation (k-ε model) of an angular section (periodic conditions) of the rotor and the stator at different operating points

4-month internship, in a research center in numerical methods applied for aeronautics, as an intern in the Argo team - Validation of the “Argo code”, based on the discontinuous Galerkin method- Simulations launched on the channel case (2 infinite vertical plan, reduced to a restrained region with periodic conditions), comparison on the velocity spectra and profiles of the flow with a Direct Numerical Simulation- Writing of scripts in Pyhton/C++ for the meshing, the post-treatment of the computations and also the addition of new elements types in the mesh

Douai

One-month internship working on a car assembly line as a Checkman

Tutoring secondary school students in mathematics, physics and chemistry.

Master Of Science (M.Sc.), Aerospace Engineering, Final German Grade: 2,2

Top 50 worldwide in Mechanical Engineering, Double degree with the Ecole Centrale de Nantes Aerodynamics (aircraft, turbomachinery.

Master'S Degree, Mechanical Engineering, Gpa 3.56

Top French "Grande Ecole", General Engineering School 2nd year specialization: Aeronautic (avionics, composite material, flight mechanics.

Preparatory Classes In Mpsi/Mp*, Mathematics, Physics And Chemistry. Information Technology Option.

Activities and Societies: Two years intensive undergraduate studies in physics, mathematics, industrial science, preparing.

Baccalauréat (A-Level Equivalent), Major In Maths, First Class Honours