Biblio

Found 313 results
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Submitted
Tani N, Marconcini M, Arcangeli L, Maceli N, Auciello J, Rizzi S, Arnone A.  Submitted.  Aerodynamic Design and Performance Analysis of a Multi-Stage Low Pressure Section for Geothermal Steam Turbine. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178401
Tani N, Marconcini M, Arcangeli L, Maceli N, Auciello J, Rizzi S, Arnone A.  Submitted.  Aerodynamic Design and Performance Analysis of a Multi-Stage Low Pressure Section for Geothermal Steam Turbine. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178401
Tani N, Marconcini M, Arcangeli L, Maceli N, Auciello J, Rizzi S, Arnone A.  Submitted.  Aerodynamic Design and Performance Analysis of a Multi-Stage Low Pressure Section for Geothermal Steam Turbine. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178401
Masi E, Nesi F, Batisti M, Bicchi M, Belardini E, Grimaldi A, Marconcini M, Arnone A.  Submitted.  Critical Analysis of Simplified Volute Models for Single-Stage Centrifugal Compressors. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
Pela A, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Valente R, Arnone A.  Submitted.  Expanding the Continuous Generation of a Family of High-Mach Number Centrifugal Compressor Stages. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178425
Pela A, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Valente R, Arnone A.  Submitted.  Expanding the Continuous Generation of a Family of High-Mach Number Centrifugal Compressor Stages. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178425
Peruzzi L, Bandini A, Bettini C, Marconcini M, Arnone A.  Submitted.  Impact of Unsteady Full-Annulus Cfd on the Predictions of High-Pressure Turbine Thermal Loads: A Comparative Study With Steady State Mixing-Plane Approach. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
Batisti M, Marconcini M, Pinelli L, Arnone A, Agnolucci A, Belardini E, D'Urso F, Grimaldi A, Valente R.  Submitted.  Integrated Aero-Structural Optimization of a New Family of Transonic Centrifugal Compressor Impellers. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178109
Batisti M, Marconcini M, Pinelli L, Arnone A, Agnolucci A, Belardini E, D'Urso F, Grimaldi A, Valente R.  Submitted.  Integrated Aero-Structural Optimization of a New Family of Transonic Centrifugal Compressor Impellers. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178109
Pela A, Bicchi M, Belardini E, Grimaldi A, Marconcini M, Arnone A.  Submitted.  Loss-Based Optimization of Static Components in Single-Stage Centrifugal Compressors. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
GT2026-178544
Toni L, Grimaldi A, Agnolucci A, Malcaus M, Batisti M, Marconcini M, Arnone A.  Submitted.  Towards a Paradigm Shift in Centrifugal Compressor Architecture: Assessment of a Multistage Rotor Equipped With Forward and Back-Swept Impellers. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
Toni L, Grimaldi A, Agnolucci A, Malcaus M, Batisti M, Marconcini M, Arnone A.  Submitted.  Towards a Paradigm Shift in Centrifugal Compressor Architecture: Assessment of a Multistage Rotor Equipped With Forward and Back-Swept Impellers. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.
2025
Milli L, Lottini F, Marconcini M, Arnone A.  2025.  CFD Investigation of Unsteady Interactions in a Radial-Axial Turboexpander for Geothermal Power Plant Applications. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T35A006.
GT2025-153202
Pela A, Marconcini M, Arnone A, Agnolucci A, Belardini E, Valente R, Grimaldi A, Toni L.  2025.  Convolutional Neural Network Approach for Impeller Blade Loading Inference. 1st International Symposium on AI and Fluid Mechanics (AIFLUIDs).
Pela A, Marconcini M, Arnone A, Agnolucci A, Belardini E, Valente R, Grimaldi A, Toni L.  2025.  Convolutional Neural Network Approach for Impeller Blade Loading Inference. 1st International Symposium on AI and Fluid Mechanics (AIFLUIDs).
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  2025.  Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T35A009.
GT2025-153766. Published on ASME J. Eng. Gas Turbine. Power
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  2025.  Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T35A009.
GT2025-153766. Published on ASME J. Eng. Gas Turbine. Power
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  2025.  Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. J. Eng. Gas Turbine. Power. 147(12):121003.
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.  2025.  Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. J. Eng. Gas Turbine. Power. 147(12):121003.
Nesi F, Marconcini M, Arnone A, Girelli S, Alfani D, Silva P.  2025.  Fast Turbomachinery Design Tools for Multi-Good Plants Based on sCO2 Cycles: the MUSIC Project Experience. ATI Annual Congress (ATI 2025) . Journal of Physics: Conference Series, Volume 3143
Nesi F, Marconcini M, Arnone A, Girelli S, Alfani D, Silva P.  2025.  Fast Turbomachinery Design Tools for Multi-Good Plants Based on sCO2 Cycles: the MUSIC Project Experience. ATI Annual Congress (ATI 2025) . Journal of Physics: Conference Series, Volume 3143
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

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