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Mechanical and Aerospace Engineering

D-Index
38
Citations
4104
World Ranking
2329
National Ranking
85

Overview

Francesco Nasuti is affiliated with Sapienza University of Rome in Italy. Their research primarily spans the field of Engineering, with a particular focus on Aerospace Engineering, Computational Mechanics, and Mechanics of Materials. Additional areas of study include Applied Mathematics and Fluid Flow and Transfer Processes.

Their work covers a range of topics including:

  • Rocket and propulsion systems research
  • Heat transfer and supercritical fluids
  • Energetic Materials and Combustion
  • Computational Fluid Dynamics and Aerodynamics
  • Gas Dynamics and Kinetic Theory
  • Combustion and flame dynamics
  • Aerospace Engineering and Control Systems

Recent papers authored by Francesco Nasuti include:

  • Pseudo-boiling and heat transfer deterioration while heating supercritical liquid rocket engine propellants, 2020, The Journal of Supercritical Fluids
  • Conjugate heat transfer analysis of rectangular cooling channels using modeled and direct numerical simulation of turbulence, 2021, International Journal of Heat and Mass Transfer

Frequent co-authors in their publications include:

  • Daniele Bianchi
  • Mario Tindaro Migliorino
  • Marco Pizzarelli
  • Enrico Cavallini
  • Matteo Fiore

Francesco Nasuti's research has been published in several prominent venues such as:

  • Journal of Propulsion and Power
  • Aerospace Science and Technology
  • Aerotecnica Missili & Spazio
  • AIAA Propulsion and Energy 2021 Forum
  • AIAA SCITECH 2023 Forum

Best Publications

  • Material-dependent catalytic recombination modeling for hypersonic flows

    Francesco Nasuti;Maurizio Barbato;Claudio Bruno

  • Numerical analysis of deterioration in heat transfer to near-critical rocket propellants

    M. Pizzarelli;A. Urbano;F. Nasuti

  • Numerical Analysis of Nozzle Material Thermochemical Erosion in Hybrid Rocket Engines

    Daniele Bianchi;Francesco Nasuti

  • Numerical Analysis of Three-Dimensional Flow of Supercritical Fluid in Cooling Channels

    Marco Pizzarelli;Francesco Nasuti;Renato Paciorri;Marcello Onofri

  • Onset of Heat Transfer Deterioration in Supercritical Methane Flow Channels

    Annafederica Urbano;Francesco Nasuti

  • Chemical erosion of carbon-phenolic rocket nozzles with finite-rate surface chemistry

    Daniele Bianchi;Alessandro Turchi;Francesco Nasuti;Marcello Onofri

  • Thermochemical erosion analysis for graphite/carbon-carbon rocket nozzles

    Daniele Bianchi;Francesco Nasuti;Marcello Onofri;Emanuele Martelli

  • Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles

    Daniele Bianchi;Francesco Nasuti;Emanuele Martelli

  • Coupled Wall Heat Conduction and Coolant Flow Analysis for Liquid Rocket Engines

    Marco Pizzarelli;Francesco Nasuti;Marcello Onofri

  • Role of Wall Shape on the Transition in Axisymmetric Dual-Bell Nozzles

    Francesco Nasuti;Marcello Onofri;Emanuele Martelli

  • Analysis of unsteady supersonic viscous flows by a shock-fitting technique

    F. Nasuti;M. Onofri

  • CFD analysis of transcritical methane in rocket engine cooling channels

    Marco Pizzarelli;Francesco Nasuti;Marcello Onofri

  • Shock structure in separated nozzle flows

    Francesco Nasuti;Marcello Onofri

  • Navier-Stokes Simulations of Hypersonic Flows with Coupled Graphite Ablation

    Daniele Bianchi;Francesco Nasuti;Emanuele Martelli

  • Numerical Parametric Analysis of Dual-Bell Nozzle Flows

    Emanuele Martelli;Francesco Nasuti;Marcello Onofri

  • Analysis of In-Flight Behavior of Truncated Plug Nozzles

    F. Nasuti;M. Onofri

  • Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles

    F. Nasuti;M. Onofri

  • Carbon-Carbon Nozzle Erosion and Shape Change in Full-Scale Solid-Rocket Motors

    Daniele Bianchi;Francesco Nasuti

  • Hybrid Rockets with Axial Injector: Port Diameter Effect on Fuel Regression Rate

    Daniele Bianchi;Francesco Nasuti;Carmine Carmicino

  • Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels

    Marco Pizzarelli;Francesco Nasuti;Marcello Onofri;Pietro Roncioni

  • PLUG NOZZLES: SUMMARY OF FLOW FEATURES AND ENGINE PERFORMANCE

    Marcello Onofri;M Calabro;G Hagemann;H Immich

  • Numerical Analysis of Three-Dimensional Flow of Supercritical Fluid in Asymmetrically Heated Channels

    Marco Pizzarelli;Francesco Nasuti;Renato Paciorri;Marcello Onofri

Frequent Co-Authors

Matteo Bernardini
Matteo Bernardini Sapienza University of Rome
Vigor Yang
Vigor Yang Georgia Institute of Technology
Brian J. Cantwell
Brian J. Cantwell Stanford University

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