Engin Ünal

Research & Testing Manager at Kenda Tires

Greater Hamburg Area

About

Experience

  • Kenda Tires (Full-time · 6 yrs)
    • Research & Testing Manager
      Jan 2024 - Present · 2 yrs 7 mos

    • Research & Testing Team Leader
      Mar 2021 - Feb 2024 · 3 yrs

    • Senior Engineer / CAE Expert
      Aug 2020 - Mar 2021 · 8 mos

  • Team Leader Stress / CAE Expert at Altran Deutschland S.A.S. & Co. KG
    Jan 2018 - Jul 2020 · 2 yrs 7 mos

  • Calculations Team Leader at Ferchau Engineering Aviation Division
    May 2011 - Dec 2017 · 6 yrs 8 mos

    Administrative and Project Management Experience in: Reference development for potential customers Effort forecasts and technical offer preparation Project monitoring Check list preparation and quality monitoring Leading multinational teams up to 20 engineers Motivating and mentoring team members Conducting internal trainings Preparing weekly reports of team loading and capacity forecasts Creating analysis methodology documents Conducting interviews with potential candidates Managing the infrastructure requirements in terms of hardware and software Ensuring optimum utilization of resources Supervising and management of the offshore and nearshore suppliers Hands-on Technical Experience in: Linear and Non-Linear Structural Analyses Topology, Topography, Shape and Size Optimizations Dynamic Transient Structural Analyses Transient Thermal Analyses Multi-body Dynamics Fatigue Analyses Computational Fluid Dynamics Tool Experience: MSC Nastran/Patran MSC Marc/Mentat Abaqus CAE Ansys WB Fluent HyperMesh/View Optistruct Radioss Hypercrash MotionSolve/View Catia V5 ISAMI Involved technical projects are listed in the "Projects" section in detail.

  • Stress Engineer at Korea Aerospace Industries, Ltd.
    Apr 2010 - May 2011 · 1 yr 2 mos

    FE Model creation and validation of Centre Wing Box DFEM for A350XWB-900. DFEM creation by using GFEM of center wing box. Validation of DFEM acc. to AM2036 and validation report writing. Static sizing of wing ribs and fuel tank boundary diaphragms of A350XWB-900 for C-Maturity. Justification of Ribs and FTBD under Material Strength, Filled Hole, Inter-River Buckling, Global Buckling, Local Buckling, Pressure Panel, Section Strength failure modes. C-Maturity report writing. Analysis Type: Linear Static Structural Toolset: Altair HyperMesh/View MSC Nastran/Patran Hand Calculations

  • CAE Engineer & Team Leader at ZF Lemfoerder
    Apr 2005 - Apr 2010 · 5 yrs 1 mo

    Linear static and non-linear static justification of suspension system parts such as subframes, control arms, knuckles, Tie Rods and Ball Joints Justification of shifters, shifter boxes and brake pedals. Topology and size optimization of suspension system components. Sealing boot non-linear sealing force analyses. Toolset: Altair HyperMesh/View Altair Optistruct MSC Marc/Mentat MSC Nastran/Patran Catia V5