Biblio

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.

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.

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.

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.

Pinelli L, Biagini P, Marconcini M, Mushtaq N, Gaetani P.  Submitted.  Impact of Rotating Detonation Combustor Shock Wave Patterns on Supersonic Inlet Turbine Stage Performance. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.

Pinelli L, Biagini P, Marconcini M, Mushtaq N, Gaetani P.  Submitted.  Impact of Rotating Detonation Combustor Shock Wave Patterns on Supersonic Inlet Turbine Stage Performance. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.

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, Agnolucci A, Belardini E, D'Urso F, Grimaldi A, Valente R, Arnone A.  Submitted.  Integrated Aero-Structural Optimization of a New Family of Transonic Centrifugal Compressor Impellers. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.

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.

Pinelli L, Bettini C, Bandini A, Carretta M, Marconcini M.  Submitted.  Modeling Low Engine Order Vibrations on Last Stage Blade of Steam Turbines Operating at Low Volumetric Flow. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.

Metti L, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  Submitted.  Multi-Fidelity Study of Secondary Flow and Transition in the SPLEEN Cascade With Endwalls. ASME Turbo Expo 2026 Turbomachinery Technical Conference and Exposition.

Metti L, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  Submitted.  Multi-Fidelity Study of Secondary Flow and Transition in the SPLEEN Cascade With Endwalls. 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.

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.

Fang Y, Reissmann M, Pacciani R, Zhao Y, Ooi ASH, Marconcini M, Akolekar HD, Sandberg R.  2026.  Accelerating CFD-Driven Training of Transition and Turbulence Models for Turbine Flows By One-Shot and Real-Time Transformer Integration. Computers & Fluids. 306

Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2026.  The Impact of Transition and Turbulence Modeling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME J Turbomach. 148(2):021011.

Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2026.  The Impact of Transition and Turbulence Modeling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME J Turbomach. 148(2):021011.

Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2026.  The Impact of Transition and Turbulence Modeling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME J Turbomach. 148(2):021011.

Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A, Spano E, Bertini F.  2026.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part II: Effect of Reynolds Number on Different Blade Geometries. ASME J Turbomach. 148(7):071002.

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 I: Computational Opportunities and Methodology. ASME J Turbomach. 148(7):071001.

Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.

Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.

Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)

Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)