Conference Paper
Arnone A, Pacciani R.
1997.
Numerical Prediction of Trailing Edge Wake Shedding. ASME Turbo Expo.
June 2–5, Orlando, FL, USA, ASME paper 97-GT-89
Steinthorsson E, Liou MS, Povinelli LA, Arnone A.
1993.
Numerical Simulation of Three-Dimensional Laminar Flow Over a Backward Facing Step; Flow Near Side Walls. ASME Fluids Engineering Division Conference, Symposium on Separated Flows. 149:19-26.
Washington, D.C., June 20-24 (NASA TM-106248, ICOMP-93-21)
Bicchi M, Pinelli L, Marconcini M, Gaetani P, Persico G.
2019.
Numerical Study of a High-Pressure Turbine Stage with Inlet Distortions. 74TH ATI NATIONAL CONGRESS: Energy Conversion: Research, Innovation and Development for Industry and Territories. AIP Conference Proceedings vol. 2191:020020.
Bicchi M, Pinelli L, Marconcini M, Gaetani P, Persico G.
2019.
Numerical Study of a High-Pressure Turbine Stage with Inlet Distortions. 74TH ATI NATIONAL CONGRESS: Energy Conversion: Research, Innovation and Development for Industry and Territories. AIP Conference Proceedings vol. 2191:020020.
Pinelli L, Poli F, Arnone A, Schipani C.
2009.
A Time-Accurate 3D Method for Turbomachinery Blade Flutter Analysis. 12th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 1–4, London, UK. paper I12-S8-3
Pinelli L, Poli F, Arnone A, Schipani C.
2009.
A Time-Accurate 3D Method for Turbomachinery Blade Flutter Analysis. 12th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 1–4, London, UK. paper I12-S8-3
Boccini E, Meli E, Rindi AA, Pinelli L, Peruzzi L, Arnone A.
2018.
Towards structural topology optimization of rotor blisks. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 7A: Structures and Dynamics:pp.V07AT30A008;10pages.
paper GT2018-76482
Boccini E, Meli E, Rindi AA, Pinelli L, Peruzzi L, Arnone A.
2018.
Towards structural topology optimization of rotor blisks. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 7A: Structures and Dynamics:pp.V07AT30A008;10pages.
paper GT2018-76482
Arnone A, Cattanei A, Nurzia F, Pacciani R, Zunino P.
2000.
A Two-Stage Low Pressure Gas-Turbine Model for Rotor-Stator Aerodynamic Interaction Investigations. XV Symposium of Measurement Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines.
Firenze, Italy, September 2000