Edoardo Scoletta

PhD | Early Stage Researcher in EU POLKA project at Technical University Munich
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Contact Information
us****@****om
(386) 825-5501
Location
DE
Languages
  • Italian Native or bilingual proficiency
  • English Full professional proficiency
  • French Professional working proficiency
  • German Elementary proficiency
Skills

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Credentials

  • IELTS (International English Language Testing System)
    British Council
    Dec, 2015
    - Oct, 2024

Experience

  • Technical University of Munich
    • Germany
    • Research Services
    • 700 & Above Employee
    • PhD | Early Stage Researcher in EU POLKA project
      • Sep 2019 - Present

      Research topic on thermoacoustic instabilities in combustion systems, further understanding and modelling of flame dynamics of hydrogen fuel blends. - CFD simulations for frequency responses of enriched H2 flames - thermoacoustic stability analyses via network-models - development of low-order-models for the impact of hydrogen enrichment on H2/CH4 conical laminar flames Research topic on thermoacoustic instabilities in combustion systems, further understanding and modelling of flame dynamics of hydrogen fuel blends. - CFD simulations for frequency responses of enriched H2 flames - thermoacoustic stability analyses via network-models - development of low-order-models for the impact of hydrogen enrichment on H2/CH4 conical laminar flames

  • ArianeGroup
    • France
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Master Thesis Project
      • Apr 2018 - Sep 2018

      The Orion Multi-Purpose Crew Vehicle (MPCV) is a US-spacecraft currently under development by NASA designed to support crewed long-duration deep space missions. Thesis goals: - Improvements of 1D hydraulic transient simulations for Propellant Feeding System by reproduction of localised gaseous Helium - Conception and solver implementation of alternative approach for multi-phase, multi-flow numerical simulations The Orion Multi-Purpose Crew Vehicle (MPCV) is a US-spacecraft currently under development by NASA designed to support crewed long-duration deep space missions. Thesis goals: - Improvements of 1D hydraulic transient simulations for Propellant Feeding System by reproduction of localised gaseous Helium - Conception and solver implementation of alternative approach for multi-phase, multi-flow numerical simulations

  • European Space Agency - ESA
    • France
    • Space Research and Technology
    • 700 & Above Employee
    • ESA Academy - Concurrent Engineering Challenge 2017
      • Sep 2017 - Sep 2017

  • Pprime
    • France
    • Research
    • 1 - 100 Employee
    • Intern - “Closed loop flat plate pulsating heat pipe for space application”
      • Jun 2017 - Sep 2017

      - performance analysis of PHPs on the "edge-configuration", comparing experimental data with the numerical results from a developed 1D Matlab model - design and development of PHP for ESA Parabolic Flight Campaign April 2018 - performance analysis of PHPs on the "edge-configuration", comparing experimental data with the numerical results from a developed 1D Matlab model - design and development of PHP for ESA Parabolic Flight Campaign April 2018

Education

  • Technical University Munich
    Doctor of Philosophy - PhD, Mechanical Engineering, Thermo-Fluid Dynamics
    2019 - 2022
  • Ecole nationale supérieure de Mécanique et d'Aérotechnique
    Master of Science in Aeronautical Mechanics and Energetics (AME), Major of Energetics and Propulsion
    2016 - 2018
  • Politecnico di Milano
    Bachelor’s Degree, Aerospace Engineering
    2012 - 2016
  • Atlantic Language Dublin
    IELTS Preparation Exam
    2015 - 2015

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