Biblio

Found 35 results
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Submitted
Pela A, Marconcini M, Arnone A, Agnolucci A, Toni L, Belardini E, Valente R, Grimaldi A.  Submitted.  Convolutional Neural Network Approach for Impeller Blade Loading Inference. 1st International Symposium on AI and Fluid Mechanics (AIFLUIDs).
In Press
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  In Press.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition.
GT2025-153843
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  In Press.  Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition.
GT2025-153766
Pela A, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  In Press.  Towards the Automatic Generation of Transonic Centrifugal Impellers by Deep Learning and Feature Importance Techniques. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition.
GT2025-153947
2024
Pela A, Marconcini M, Arnone A, Agnolucci A, Toni L, Valente R, Belardini E.  2024.  Exploiting Deep Learning for the Optimization of Transonic Centrifugal Impellers. Journal of Physics Conference Series - 79th ATI National Conference. 2893
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)
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
2023
Savio P, Scionti A, Vitali G, Viviani P, Vercellino C, Terzo O, Nguyen H-N, Magarielli D, Spano E, Marconcini M et al..  2023.  Accelerating Legacy Applications with Spatial Computing Devices. Journal of Supercomputing. 79:7461–7483.
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
Pela A, Marconcini M, Arnone A, Toni L, Valente R, Agnolucci A, Grimaldi A, Pacciani R.  2023.  On the Feasibility of Helicity-Based Corrections of Turbulence Models for Improving RANS Predictions of Centrifugal Compressor Stages. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13D: Turbomachinery
GT2023-103852
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
Bicchi M, Marconcini M, Bellobuono E F, Belardini E, Toni L, Arnone A.  2023.  Multi-Point Surrogate-Based Approach for Assessing Impacts of Geometric Variations on Centrifugal Compressor Performance. Energies. 16:1584.
Agnolucci A, Marconcini M, Biliotti D, Toni L, Baroni A, Romani L, Arnone A.  2023.  Robust Design of a Vaned Diffuser in a Centrifugal Compressor Stage With a High Load Impeller. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13D: Turbomachinery
GT2023-103585
Bicchi M, Biliotti D, Toni L, Marconcini M, Grimaldi A, Arnone A.  2023.  A Two-Step Approach for Centrifugal Compressor Performance Mapping Based on a Reduced-Order Model and an Evolutionary Algorithm. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13D: Turbomachinery
GT2023-102252
2022
Bicchi M, Biliotti D, Marconcini M, Toni L, Cangioli F, Arnone A.  2022.  An AI-Based Fast Design Method for New Centrifugal Compressor Families. Machines. 10(6)
Lottini F, Agnolucci A, Pinelli L, Pacciani R, Toni L, Guglielmo A, Grimaldi A.  2022.  Impact of Operating Conditions on Rotor/Stator Interaction of a High-Pressure Ratio Centrifugal Compressor. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. Volume 10B: Turbomachinery
ASME paper GT2022-82108
Lottini F, Marconcini M, Biliotti D, Toni L, Arnone A.  2022.  Numerical Investigation on Radial Turbines Aerodynamics Aimed at the Definition of Design Rules for Industrial Applications. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. Volume 10B: Turbomachinery
ASME paper GT2022-82266
2021
Agnolucci A, Marconcini M, Arnone A, Toni L, Grimaldi A, Giachi M.  2021.  Centrifugal Compressor Stage Efficiency and Rotor Stiffness Augmentation via Artificial Neural Networks. ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition. 2D: Turbomachinery: Radial Turbomachinery Aerodynamics
ASME paper GT2021-59998
2019
Biagiotti S, Bellucci J, Marconcini M, Arnone A, Baldi G, Ignesti M, Michelassi V, Tapinassi L.  2019.  Impact of Turbine Center Frame Wakes on Downstream Rows in Heavy Duty Free Power Turbine. ASME Turbo Expo 2019. Volume 2A: Turbomachinery:V02AT45A007.
ASME paper GT2019-90721
2018
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.
Pinelli L, Vanti F, Arnone A, Eret P, Tsymbalyuk V, Lo Balbo A A.  2018.  Numerical and Experimental Assessment of Flutter Stability in a Turbine Linear Cascade. 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
paper ISUAAAT15-029

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