Biblio

Poli F, Marconcini M, Pacciani R, Arnone A, Magarielli D, Spano E.  2022.  Exploiting GPU-based HPC Architectures to Accelerate an Unsteady CFD Solver for Turbomachinery Applications. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. Volume 10C: Turbomachinery

Poli F, Arnone A, Schipani C.  2009.  A 3D Linearized Method for Turbomachinery Tone Noise Analysis With 3D Non-Reflecting Boundary Conditions. 8th European Turbomachinery Conference (ETC8). :713-722.

Poli F, Gambini E, Arnone A, Schipani C.  2006.  A 3D Time-Linearized Method for Turbomachinery Blade Flutter Analysis. 11th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).

Poli F, Pinelli L, Arnone A.  2015.  Aeroelastic Stability Analysis of a Non-Rotating Annular Turbine Test Rig: a Comparison Between a Linearized and a Non-Linear Computational Method. 22nd International Congress on Sound and Vibration, (ICSV22).

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  The Effect of Entropy Waves Features on the Indirect Noise Generation within an Aeronautical High Pressure Turbine Stage. Journal of Physics Conference Series - 79th ATI National Conference. 2893

Pinelli L, Burberi C, Ignesti M, Michelassi V, Tapinassi L, Abati A, Pacciani R.  2023.  Forced response in a multi-stage aeroderivative axial compressor with acoustic excitations: Method validation with field data. Aerospace Science and Technology. 138

Pinelli L, Poli F, Marconcini M, Arnone A, Schipani C, Spano E, Torzo D.  2011.  A Linearized Method for Tone Noise Generation and Propagation Analysis in a Multistage Contra-Rotating Turbine. 9th European Turbomachinery Conference (ETC9). :1253–1263.

Pinelli L, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2022.  The Effects of Swirling Flows In Entropy Wave Convection Through High Pressure Turbine Stage. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. 10D: Turbomachinery

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage. ASME J. Turbomach.. 146(4):041003.

Pinelli L, Malcaus M, Giannini G, Marconcini M.  In Press.  Some Experiences About the RANS Modeling of UHBR Fan: The Case of ECL5/CATANA. Int. J. Turbomach. Propuls. Power..

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).

Pinelli L, Amedei A, Meli E, Vanti F, Romani B, Benvenuti G, Fabbrini M, Morganti N, Rindi A, Arnone A.  2022.  Innovative Design, Structural Optimization and Additive Manufacturing of New-Generation Turbine Blades. ASME J. Turbomach.. 144(1):011006.

Pinelli L, Vienni D, Tapinassi L, Michelassi V, Burberi C, Lorusso S, Ignesti M, Marconcini M.  2024.  Understanding the Aerodynamic Damping Behavior of an Axial Compressor Rotor for Industrial Applications. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 10A: Structures and Dynamics:V10AT21A016.

Pinelli L, Poli F, Arnone A, Guérin S, Holewa A, Aparicio JRFernán, Puente R, Torzo D, Favre C, Gaetani P et al..  2015.  On the Numerical Evaluation of Tone Noise Emissions Generated by a Turbine Stage: an In-Depth Comparison Among Different Computational Methods. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. 2B: Turbomachinery

Pinelli L, Marconcini M, Pacciani R, Gaetani P, Persico G.  2021.  Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High Pressure Turbine Stage. ASME J. Turbomach.. 143(9)

Pinelli L, Poli F, Bellucci J, Giovannini M, Arnone A.  2015.  Evaluation of Fast Numerical Methods for Turbomachinery Blade Flutter Analysis. 14th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).

Pinelli L, Vanti F, Arnone A, Bessling B, Vogt D.  2019.  Influence of tip shroud modeling on the flutter stability of a low pressure turbine rotor. ASME Turbo Expo 2019. Volume 7A: Structures and Dynamics:V07AT36A012.

Pinelli L, Marconcini M, Pacciani R, Bake F, Knobloch K, Gaetani P, Persico G.  2022.  Effect of Clocking on Entropy Noise Generation Within an Aeronautical High Pressure Turbine Stage. J.Sound Vib.. 529(116900)

Pinelli L, Malcaus M, Giannini G, Marconcini M.  2025.  Some Experiences About the RANS Modeling of UHBR Fan: The Case of ECL5/CATANA. 16th European Turbomachinery Conference ETC16.

Pinelli L, Lilli L, Arnone A, Gaetani P, Persico G.  2020.  Numerical Study of Entropy Wave Evolution within a HPT Stage. 75th National ATI Congress – #7 Clean Energy for all (ATI 2020). E3S Web Conf. Volume 197:11011(12).

Pinelli L, Mariotti F, Arnone A, Marconcini M, Arcangeli L, Ciuchicchi L, Maceli N.  2022.  Numerical Investigation of Potential Flow Induced Vibrations of Steam Turbine Last Stage Rotor at Low Load Operation – Part 1: Sensitivity to Flutter Occurrence. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. Volume 2: Coal, Biomass, Hydrogen, and Alternative Fuels

Pinelli L, Poli F, Di Grazia E, Arnone A, Torzo D.  2013.  A Comprehensive Numerical Study of Tone Noise Emissions in a Multistage Cold Flow Rig. 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference), 27-29 May.

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  Understanding Entropy Wave Evolution in High-Pressure Turbines: The Role of Hot Spot Position and Features. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery:V12DT36A015.

Pinelli L, Poli F, Di Grazia E, Arnone A, Taddei F, De Lucia M, Torzo D.  2015.  Numerical and Experimental Study of the Tone Noise Generation By a Turbine Rear Frame. 22nd International Congress on Sound and Vibration, (ICSV22).

Pinelli L, Lori F, Marconcini M, Pacciani R, Arnone A.  2021.  Validation of a Modal Work Approach for Forced Response Analysis of Bladed Disks. Applied Sciences. 11(12):5437.