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  1. Differential Throttling in Linear Aerospike: A Combined Experimental and Numerical Study

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio, Michele Ferlauto

  2. A Two-Dimensional Analysis of the Flowfield and Performances of Linear Aerospikes During Differential Throttling

    Article • Aerospace, February 2025, MDPI AG

    Dr Roberto Marsilio

  3. Innovative Concepts in the DTT Neutral Beam Injector

    Article • IEEE Transactions on Plasma Science, September 2024, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Roberto Marsilio

  4. Characterization of the Three-Dimensional Flowfield over a Truncated Linear Aerospike

    Article • Fluids, August 2024, MDPI AG

    Dr Roberto Marsilio

  5. A Framework for Testing Differential Throttling in Linear Aerospike Nozzle

    Article • June 2024, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Roberto Marsilio

  6. Passive Control of Vortices in the Wake of a Bluff Body

    Article • Fluids, May 2024, MDPI AG

    Dr Roberto Marsilio

  7. Thrust Vectoring using Differential Throttling in Axisymmetric Aerospike Nozzle

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio, Michele Ferlauto

  8. On the Use of Vortex Identification for the Optimisation of Trapped Vortex Devices

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Marek Paty, Dr Roberto Marsilio, Michele Ferlauto

  9. Numerical and experimental assessment of a linear aerospike

    Article • November 2023, Materials Research Forum, LLC

    Dr Roberto Marsilio

  10. Experimental Characterization of a Linear Aerospike Nozzle Flow

    Article • June 2023, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Roberto Marsilio

  11. Influence of Hot Flow Conditions on Nozzle Performances

    Article • January 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio

  12. Improved Conceptual Design of the Beamline for the DTT Neutral Beam Injector

    Article • IEEE Transactions on Plasma Science, November 2022, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Roberto Marsilio, Professor Domenic D'Ambrosio

  13. Cold Gas Measurement System for Linear Aerospike Nozzles

    Article • June 2022, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Roberto Marsilio

  14. Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio, Michele Ferlauto

  15. AI assisted detection of shock motions inside a transonic duct

    Article • January 2022, American Institute of Physics

    Dr Roberto Marsilio

  16. Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method

    Article • Fluids, December 2021, MDPI AG

    Dr Roberto Marsilio

  17. Numerical validation and analysis of supersonic retropropulsion test cases.

    Article • July 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Domenic D'Ambrosio, Dr Roberto Marsilio

  18. Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike

    Article • International Journal of Turbomachinery Propulsion and Power, April 2021, MDPI AG

    Dr Roberto Marsilio

  19. A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike

    Article • January 2021, Scipedia, S.L.

    Dr Roberto Marsilio

  20. Fluidic Thrust Vectoring for Annular Aerospike Nozzle

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  21. Shock Vector Control Technique for Aerospike Nozzles

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio

  22. Numerical simulation of a vectored axisymmetric nozzle

    Article • January 2020, American Institute of Physics

    Michele Ferlauto, Dr Roberto Marsilio

  23. Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  24. CFD-based Fluidic Thrust Vectoring model for fighter aircraft

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Elisa Capello, Dr Roberto Marsilio, Michele Ferlauto

  25. Computational Investigation of Injection Effects on Shock Vector Control Performance

    Article • July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  26. On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  27. A Vortex-In-Cell Method for the Simulation of Viscous Flows

    Article • International Review on Modelling and Simulations (IREMOS), October 2017, Praise Worthy Prize

    Dr Roberto Marsilio

  28. Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring

    Article • AIAA Journal, January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio, Michele Ferlauto

  29. A numerical method for the study of fluidic thrust-vectoring

    Article • Advances in aircraft and spacecraft science, October 2016, Techno-Press

    Michele Ferlauto, Dr Roberto Marsilio

  30. Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio, Michele Ferlauto

  31. Numerical Simulation of Fluidic Thrust-Vectoring

    Article • Aerotecnica Missili & Spazio, July 2016, Springer Science + Business Media

    Dr Roberto Marsilio

  32. A computational approach to the simulation of controlled flows by synthetic jets actuators

    Article • Advances in aircraft and spacecraft science, January 2015, Techno-Press

    Michele Ferlauto, Dr Roberto Marsilio

  33. A computational method for combustion in high speed flows

    Article • Computers & Fluids, November 2012, Elsevier

    Dr Roberto Marsilio

  34. A Computational Method for Combustion in Supersonic Flows

    Article • July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio

  35. Synthetic Jet Actuator Modeling for Flow Control Applications

    Article • January 2009, Springer Science + Business Media

    Michele Ferlauto, Dr Roberto Marsilio

  36. Simulation of Jet Engine Transients by a CFD Method

    Article • July 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  37. A viscous inverse method for aerodynamic design

    Article • Computers & Fluids, March 2006, Elsevier

    Michele Ferlauto, Dr Roberto Marsilio

  38. Inverse Problems for Advanced Nozzle Design

    Article • July 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  39. A 2-D Viscous Inverse Problem Method for Aerodynamics Design

    Article • June 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Michele Ferlauto, Dr Roberto Marsilio

  40. Turbulent Model Validation for Spike Nozzle External Flows

    Article • January 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio

  41. A New Set of Boundary Conditions for Aerodynamic Design

    Article • January 2003, Springer Science + Business Media

    luca zannetti, Michele Ferlauto, Dr Roberto Marsilio

  42. A numerical method for solving the three-dimensional parabolized Navier-Stokes equations

    Article • Computers & Fluids, July 1997, Elsevier

    Dr Roberto Marsilio

  43. Shock-induced separated structures in symmetric corner flows

    Article • June 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Domenic D'Ambrosio, Dr Roberto Marsilio

  44. Vortical Solutions in Supersonic Corner Flows

    Article • AIAA Journal, September 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Roberto Marsilio

  45. Shock-fitting method for two-dimensional inviscid, steady supersonic flows in ducts

    Article • Meccanica, December 1989, Springer Science + Business Media

    Dr Roberto Marsilio