Biblio

Found 295 results
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A
Arnone A, Carnevale E A, Marconcini M.  1997.  Grid Dependency Study for the NASA Rotor 37 Compressor Blade. ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A056;(9pages).
Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2001.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Turbo Expo 2001: Power for Land, Sea, and Air. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A008;9pages.
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
Arnone A, Benvenuti E.  1994.  Three–Dimensional Navier–Stokes Analysis of a Two–Stage Gas Turbine. ASME Turbo Expo.
The Hague, The Netherlands, June 13–16, ASME paper 94–GT–88
Arnone A.  1986.  Miglioramenti nella Risoluzione di Flussi a Potenziale nelle Turbomacchine Tramite Elementi Finiti. 41o Congresso Nazionale ATI.
23-26 September, Napoli, Italy
Arnone A, Carnevale E A, Marconcini M.  1996.  Sul Calcolo Viscoso nei Compressori Assiali Transonici. Convegno Turbomacchine '96 – Conference Proceedings. :147–157.
11-12 Luglio, Genova, Italy
Arnone A, Poli F, Schipani C.  2003.  A Method to Assess Flutter Stability of Complex Modes. 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 7–11, Durham, NC, USA
Arnone A, Stecco SS.  1991.  Transonic Cascade Flow Prediction Using the Navier-Stokes Equations. IGTI International Gas Turbine and Aeroengine Congress and Exposition.
Orlando, FL, USA, 3-6 June, 1991, ASME paper 91-GT-313
Arnone A, Boncinelli P, Munari A, Spano E.  1999.  Application of CFD Techniques to the Design of the Ariane 5 Turbopump. 14th Computational Fluid Dynamics Conference.
June 28 July 1, Norfolk, VA, USA, AIAA paper 99-3380
Arnone A, Swanson RC.  1993.  A Navier–Stokes Solver for Turbomachinery Applications. ASME Journal of Turbomachinery. 115(2):305–313.
Arnone A, Boncinelli P, Avalle M, Capuani A, Spano E.  2001.  Aerodynamic Design of the Upper Stage Ariane 5 LOX Turbopump Using CFD Techniques. 4th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics. :607–617.
20-23 March, Firenze, Italy, ATI-CST-051/01
Arnone A, Pacciani R, Sestini A.  1995.  Multigrid Computations of Unsteady Rotor–Stator Interaction Using the Navier–Stokes Equations. Journal of Fluids Engineering. 117(4):647–652.
Arnone A, Bonaiuti D, Focacci A, Pacciani R, Scotti Del Greco A, Spano E.  2004.  Parametric Optimization of a High-Lift Turbine Vane. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1469–1479.
June 14–17, Vienna, Austria, ASME paper GT2004-54308
Arnone A, Stecco SS.  1989.  Inviscid Cascade Flow Calculations Using a Multigrid Method. IGTI International Gas Turbine and Aeroengine Congress and Exposition.
Toronto, Ontario, Canada, 4-8 June, 1989, ASME paper 89-GT-22
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
Arnone A, Liou MS, Povinelli LA.  1992.  Navier–Stokes Solution of Transonic Cascade Flow Using Non–Periodic C–Type Grids. Journal of Propulsion and Power. 8(2):410–417.
B
Bandini A, Cascino A, Meli E, Pinelli L, Marconcini M.  2024.  Improving Aeromechanical Performance of Compressor Rotor Blisk With Topology Optimization. Energies. 17(8):1883.
Bandini A, Bettini C, Peruzzi L, Caretta M, Canelli C, Marconcini M, Pinelli L, Arnone A.  2024.  Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12B: Turbomachinery:V12BT30A043.
GT2024-128743 (accepted for publication on ASME Journal of Turbomachinery)
Bandini A, Bettini C, Peruzzi L, Caretta M, Canelli C, Marconcini M, Pinelli L, Arnone A.  In Press.  Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics. ASME J Turbomach.
Baroni A, Catalani I, Romani L, Bicchi M, Balduzzi F, Marconcini M, Bianchini A, Arnone A, Ferrara G, Toni L et al..  2023.  A Critical Analysis on the Impact of External Losses on the Performance of a Centrifugal Compressor Stage – Experimental and Multi-Fidelity Numerical Assessment. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13D: Turbomachinery
GT2023-102488
Barreca P, Pinelli L, Vanti F, Arnone A.  2018.  Aeroelastic Investigation of a Transonic Compressor Rotor with Multi-Row Effects. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:58-65.
Batisti M, Pinelli L, Toni L, Guglielmo A, Marconcini M, Arnone A.  In Press.  Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis. ASME J Turbomach.
Batisti M, Pinelli L, Toni L, Guglielmo A, Marconcini M, Arnone A.  2024.  Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery :V12DT35A025.
GT2024-128815  (accepted for publication on ASME Journal of Turbomachinery)
Becciani M, Bianchini A, Checcucci M, Ferrari L, De Luca M, Marmorini L, Arnone A, Ferrara G.  2017.  A Pre-Design Model to Estimate the Effect of Variable Inlet Guide Vanes on the Performance Map of a Centrifugal Compressor for Automotive Applications. 13th International Conference on Engines & Vehicles.
SAE Technical Paper 2017-24-0020
Bellucci J, Rubechini F, Marconcini M, Arnone A, Arcangeli L, Maceli N, Dossena V.  2015.  The Influence of Roughness on a High-Pressure Steam Turbine Stage: an Experimental and Numerical Study. ASME Journal of Engineering for Gas Turbines and Power. 137(1):1-9.

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