Filippo Masseni

Ph.D. in Ingegneria Aerospaziale , 32nd cycle (2016-2019)

Ph.D. obtained in 2020

Dissertation:

Optimization Approaches Under Uncertainty for Hybrid Rocket Engines (Abstract)

Tutors:

Dario Giuseppe Pastrone Lorenzo Casalino

Profile

Research interests

Combustion instability
Coupled propulsion/trajectory optimization
Hybrid rocket engines
Multidisciplinary design optimization
Robust optimization
Solid propellant

Scientific branch

ING-IND/07 - AEROSPACE PROPULSION
(Area 0009 - Industrial and information engineering)

Teaching

Collegi of the degree programmes

Teachings

Master of Science

MostraNascondi A.A. passati

Research

Research groups

Supervised PhD students

  • Leonardo Stumpo. Programme in Ingegneria Aerospaziale (cycle 39, 2023-in progress)
    Research subject: Innovative Space Propulsion Design Techniques
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
  • Alessandra Zumbo. Programme in Ingegneria Aerospaziale (cycle 39, 2023-in progress)
    Research subject: LH2 Fuel Systems for Aerospace Applications
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbomachinery
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbomachinery
    Advanced Aerospace Propulsion
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbomachinery
  • Lorenzo Folcarelli. Programme in Ingegneria Aerospaziale (cycle 38, 2022-in progress)
    Research subject: Direct Hydrogen Combustion in Jet Engines; Low-Frequency Instability in Hybrid Rockets Engines.
    Advanced Aerospace Propulsion
    Aircraft Parameter Estimation
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
    Advanced Aerospace Propulsion
    Aircraft Parameter Estimation
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
    Advanced Aerospace Propulsion
    Aircraft Parameter Estimation
    Computational Fluid Dynamics
    Propellants and Combustion
    Turbulent Flows
  • Giovanni Polizzi. Programme in Ingegneria Aerospaziale (cycle 38, 2022-in progress)

Publications

Works published during the Ph.D. View all publications in Porto@Iris