Biblio

Found 327 results
[ Author(Asc)] Keyword Type Year
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Rubechini F, Schneider A, Arnone A, Cecchi S, Malavasi F.  2011.  A Redesign Strategy to Improve the Efficiency of a 17-Stage Steam Turbine. ASME Journal of Turbomachinery. 134(3):031021.
Rubechini F, Marconcini M, Arnone A, Maritano M, Cecchi S.  2006.  The Impact of Gas Modeling in the Numerical Analysis of a Multistage Gas Turbine. ASME Turbo Expo 2006: Power for Land, Sea, and Air. 6: Turbomachinery, Parts A and B:531-539.
Rubechini F, Marconcini M, Arnone A, Cecchi S, Daccà F.  2007.  Some Aspects of CFD Modeling in the Analysis of a Low-Pressure Steam Turbine. ASME Turbo Expo. 6: Turbomachinery, Parts A and B:519–526.
ASME paper GT2007-27235
Rubechini F, Marconcini M, Arnone A, Maritano M, Cecchi S.  2008.  The Impact of Gas Modeling in the Numerical Analysis of a Multistage Gas Turbine. ASME Journal of Turbomachinery. 130(2):021022.
Rubechini F, Schneider A, Arnone A, Daccà F, Canelli C, Garibaldi P.  2011.  Aerodynamic Redesigning of an Industrial Gas Turbine. ASME Turbo Expo. 7: Turbomachinery, Parts A, B, and C :1387-1394.
Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A.  2025.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 1: Computational Opportunities and Methodology. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 11: Turbomachinery:V011T32A014.
GT2025-152583. Recommended for publication on ASME J. Turbomach.
Rosenzweig M, Giaccherini S, Pinelli L, Kozul M, Sandberg R, Marconcini M, Pacciani R.  2023.  Best-Practice Guidelines for High-Fidelity Simulations Based on Detailed Analysis of a Highly-Loaded Low-Pressure Turbine Cascade. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13B: Turbomachinery
GT2023-102697
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.
Rosenzweig M, Kozul M, Sandberg R, Marconcini M, Pacciani R.  2023.  High-Fidelity Simulations and Rans Analysis of a Low-Pressure Turbine Cascade in a Spanwise-Diverging Gas Path - End-Wall Flow Analysis and Loss Generation Mechanisms. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13B: Turbomachinery
GT2023-101039
Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A, Spano E, Bertini F.  2025.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 2: Effect of Reynolds Number on Different Blade Geometries. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 11: Turbomachinery:V011T32A024.
GT2025-153512. Recommended for publication on ASME J. Turbomach.
Romei A, Persico G, Biliotti D, Milani A, Lottini F, Marconcini M.  2023.  Design of Compact Radial Turboexpanders for sCO2 Power Systems. The European sCO2 Conference for Energy Systems.
Riccietti E, Bellucci J, Checcucci M, Marconcini M, Arnone A.  2018.  Support Vector Machine Classification Applied to the Parametric Design of Centrifugal Pumps. Engineering Optimization. 50(8):1304-1324.
Ricci M, Pacciani R, Marconcini M, Arnone A.  2020.  Prediction of Tip Leakage Vortex Dynamics in an Axial Compressor Cascade Using RANS Analyses. ASME Turbo Expo 2020 Turbomachinery Technical Conference and Exposition. 2C: Turbomachinery:12.
GT2020-14797
Ricci M, Pacciani R, Macelloni P, Cecchi S, Bettini C, Marconcini M.  2021.  An Automated Strategy for Gas Turbines Off-Design Predictions with a CFD-based Throughflow Method. Applied Thermal Engineering. 192:116783.
Ricci M, Pacciani R, Marconcini M, Macelloni P, Cecchi S, Bettini C.  2019.  CFD-Based Throughflow Analysis of Transonic Flows in Steam Turbines. ASME Turbo Expo 2019. Volume 2C: Turbomachinery:V02CT41A021.
ASME paper GT2019-90851
Ricci M, Pacciani R, Marconcini M, Arnone A.  2021.  State-of-the-Art Throughflow Analysis of Multistage Turbines by Exploiting CFD Methods. La Termotecnica. 6:72-77.
Ricci M, Pacciani R, Marconcini M, Macelloni P, Cecchi S, Bettini C.  2019.  Computational Fluid Dynamics-Based Throughflow Analysis of Transonic Flows in Steam Turbines. ASME Journal of Turbomachinery. 141(11):111005(7pages).
Ricci M, Pacciani R, Marconcini M.  2020.  The Exploitation of CFD Legacy for the Meridional Analysis and Design of Modern Gas and Steam Turbines. 75th National ATI Congress – #7 Clean Energy for all (ATI 2020). E3S Web Conf. Volume 197:11013(10).
Ricci M, Benvenuto M, Mosele S G, Pacciani R, Marconcini M.  2022.  Impact of Compressor Flexibility Improvements on Heavy-Duty Gas Turbine for Minimum and Base Load Conditions. Energies. 15(20):7546.
Ricci M, Mosele S G, Benvenuto M, Astrua P, Pacciani R, Marconcini M.  2022.  Retrofittable Solutions Capability for Gas Turbine Compressors. Int. J. Turbomach. Propuls. Power. 7(1):3.
Ricci M, Pacciani R, Marconcini M, Arnone A.  2018.  Secondary flow and radial mixing modelling for CFD-based Through-Flow method: an axial turbine application. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:218-225.
Ricci M, Pacciani R, Marconcini M, Mosele S G, Benvenuto M, Astrua P.  2021.  Retrofittable Solutions Capability for a Gas Turbine Compressor. 14th European Conference on Turbomachinery Fluid dynamics.
paper ETC2021-613
P
Poli F, Arnone A, Schipani C.  2009.  A 3D Linearized Method for Turbomachinery Tone Noise Analysis With 3D Non-Reflecting Boundary Conditions. 8th European Turbomachinery Conference (ETC8). :713-722.
23-27 March, Graz, Austria
Poli F, Gambini E, Arnone A, Schipani C.  2006.  A 3D Time-Linearized Method for Turbomachinery Blade Flutter Analysis. 11th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 4–8, Moscow, Russia

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