Biblio

Found 120 results
Author [ Keyword(Asc)] Type Year
Filters: First Letter Of Last Name is P and Author is Lorenzo Pinelli  [Clear All Filters]
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 
Computational Fluid Dynamics (CFD)
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.
Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2023.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME J. Turbomach.. 145(8):081002.
Bandini A, Bettini C, Peruzzi L, Caretta M, Canelli C, Marconcini M, Pinelli L, Arnone A.  2025.  Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics. ASME J Turbomach. 147(7):071008.
computational aeroacoustics (CAA)
Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2023.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME J. Turbomach.. 145(8):081002.
Pinelli L, Marconcini M, Arnone A, Bacci D.  2024.  High Fidelity Modeling of Acoustic Liners For Aeronautical Applications. 34th Congress of the International Council of the Aeronautical Sciences.
combustor-HPT interaction
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.
GT2024-127446
Giannini G, Pinelli L, Pacciani R, Arnone A, Bertini F, Spano E, Marconcini M.  2025.  The Impact of Modeling Assumptions on the Hot Spots Convection Within a Cooled High-Pressure Turbine Stage. Aerospace Science and Technology. 166
CO2-mixture
Bandini A, Arcangeli L, Paggini A, Nenciolini A, Iobbi M, Pinelli L, Marconcini M, Arnone A.  2025.  An Inquiry Into the Aerodynamic and Aeromechanic Aspects on Next-Generation CO2-SO2 Power Turbines for Sustainable Applications: The Case of the Desolination Project. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 9: Structures and Dynamics:V009T28A023.
GT2025-153814
CFD
Burberi C, Ghignoni E, Pinelli L, Marconcini M.  2018.  Numerical Analysis of Direct and Indirect Noise Produced by a High Pressure Turbine Stage. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:130-137.
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.
Biagiotti S, Pinelli L, Poli F, Vanti F, Pacciani R.  2018.  Numerical Study of Flutter Stabilization in Low Pressure Turbine Rotor with Intentional Mistuning. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association.. Energy Procedia 148:98-105.
Sláma V, Rudas B, Eret P, Tsymbalyuk V, Ira J, Macalka A, Pinelli L, Vanti F, Arnone A, Lo Balbo A A.  2018.  Experimental and Numerical Study of Controlled Flutter Testing in a Linear Turbine Blade Cascade. Acta Polytechnica CTU Proceedings. Vol 20 Turbomachines 2018:98-107.
Gaetani P, Persico G, Pinelli L, Marconcini M, Pacciani R.  2020.  Computational and Experimental Study of Hot Streak Transport Within the First Stage of a Gas Turbine. ASME J. Turbomach.. 142(8):081102(11pages).
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
Centrifugal Compressors
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)
cavities
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)
Blades
Peruzzi L, Bellucci J, Pinelli L, Arnone A, Arcangeli L, Cosi L, Mazzucco M.  2016.  Numerical aerodynamic damping evaluation of high-pressure steam turbine blades for aeromechanical characterization. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. 8: Microturbines, Turbochargers and Small Turbomachines; Steam Turbines:V008T26A012;10pages.
GT2016-56378
blade vibration
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.
blade cascade
Sláma V, Rudas B, Eret P, Tsymbalyuk V, Ira J, Macalka A, Pinelli L, Vanti F, Arnone A, Lo Balbo A A.  2018.  Experimental and Numerical Study of Controlled Flutter Testing in a Linear Turbine Blade Cascade. Acta Polytechnica CTU Proceedings. Vol 20 Turbomachines 2018:98-107.
axial compressor aeromechanics
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.
GT2024-128729
axial compressor
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.
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
analytical
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)
aircraft noise
Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2023.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME J. Turbomach.. 145(8):081002.
Pinelli L, Marconcini M, Arnone A, Bacci D.  2024.  High Fidelity Modeling of Acoustic Liners For Aeronautical Applications. 34th Congress of the International Council of the Aeronautical Sciences.

Pages