Biblio

Found 285 results
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2026
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.
Toni L, Grimaldi A, Agnolucci A, Malcaus M, Batisti M, Marconcini M, Arnone A.  2026.  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.  2026.  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 
Metti L, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  2026.  Unveiling Boundary Layer Physics in the SPLEEN High-Speed LPT with Realistic Turbulent Inflow: a Wall-Resolved LES Benchmark for RANS Models. Aerospace Science and Technology. :113412.
Metti L, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  2026.  Unveiling Boundary Layer Physics in the SPLEEN High-Speed LPT with Realistic Turbulent Inflow: a Wall-Resolved LES Benchmark for RANS Models. Aerospace Science and Technology. :113412.
In Press
Pela A, Marconcini M, Agnolucci A, Bicchi M, Belardini E, Grimaldi A, Valente R, Toni L, Arnone A.  In Press.  Convolutional Neural Network Approach for Impeller Blade Loading Inference. Computers & Fluids.
Pinelli L, Biagini P, Marconcini M, Mushtaq N, Gaetani P.  In Press.  Impact of Rotating Detonation Combustor Shock Wave Patterns on Supersonic Inlet Turbine Stage Performance. ASME J Turbomach.
TURBO-26-1217
Pinelli L, Biagini P, Marconcini M, Mushtaq N, Gaetani P.  In Press.  Impact of Rotating Detonation Combustor Shock Wave Patterns on Supersonic Inlet Turbine Stage Performance. ASME J Turbomach.
TURBO-26-1217
Pinelli L, Bettini C, Bandini A, Carretta M, Marconcini M.  In Press.  Modeling Low Engine Order Vibrations on Last Stage Blade of Steam Turbines Operating at Low Volumetric Flow. Journal of Engineering for Gas Turbines and Power.
GTP-26-1385

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