Biblio

Found 313 results
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2026
Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A.  2026.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 1: Computational Opportunities and Methodology. ASME J Turbomach.
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.
GT2026-178561
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.
GT2026-178599
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, Marconcini M, Bicchi M, Belardini E, Grimaldi A, 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.
 GT2026-178103 
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.
 GT2026-178103 

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