Biblio

Found 237 results
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Spatial computing
Savio P, Scionti A, Vitali G, Viviani P, Vercellino C, Terzo O, Nguyen H-N, Magarielli D, Spano E, Marconcini M et al..  2023.  Accelerating Legacy Applications with Spatial Computing Devices. Journal of Supercomputing. 79:7461–7483.
SPLEEN
Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2025.  The Impact of Transition and Turbulence Modelling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 10: Turbomachinery:V010T30A019.
GT2025-153288. Recommended for publication on ASME J. Turbomach.
Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2025.  The Impact of Transition and Turbulence Modelling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 10: Turbomachinery:V010T30A019.
GT2025-153288. Recommended for publication on ASME J. Turbomach.
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, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  Submitted.  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.
Steam Turbine
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.
Sláma V, Rudas B, Eret P, Tsymbalyuk V, Ira J, Macalka A, Pinelli L, Vanti F, Arnone A, Lo Balbo A A.  2018.  Experimental and Numerical Study of Controlled Flutter Testing in a Linear Turbine Blade Cascade. Acta Polytechnica CTU Proceedings. Vol 20 Turbomachines 2018:98-107.
test rig
Sláma V, Rudas B, Eret P, Tsymbalyuk V, Ira J, Macalka A, Pinelli L, Vanti F, Arnone A, Lo Balbo A A.  2018.  Experimental and Numerical Study of Controlled Flutter Testing in a Linear Turbine Blade Cascade. Acta Polytechnica CTU Proceedings. Vol 20 Turbomachines 2018:98-107.
time-linearized
Arnone A, Poli F, Schipani C.  2003.  A Method to Assess Flutter Stability of Complex Modes. 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 7–11, Durham, NC, USA
Tone Noise
Boncinelli P, Marconcini M, Poli F, Arnone A, Schipani C.  2006.  Time-Linearized Quasi-3D Tone Noise Computations in Cascade Flows. ASME Turbo Expo. 6, Turbomachinery, Parts A and B:1633–1642.
ASME paper GT2006-90080
Pinelli L, Poli F, Marconcini M, Arnone A, Schipani C, Spano E, Torzo D.  2011.  A Linearized Method for Tone Noise Generation and Propagation Analysis in a Multistage Contra-Rotating Turbine. 9th European Turbomachinery Conference (ETC9). :1253–1263.
Istanbul, Turkey, 21-25 March 2011
Pinelli L, Poli F, Marconcini M, Arnone A, Schipani C, Spano E, Torzo D.  2011.  A Linearized Method for Tone Noise Generation and Propagation Analysis in a Multistage Contra-Rotating Turbine. 9th European Turbomachinery Conference (ETC9). :1253–1263.
Istanbul, Turkey, 21-25 March 2011
Pinelli L, Poli F, Marconcini M, Arnone A, Spano E, Torzo D.  2011.  Validation of a 3D Linearized Method for Turbomachinery Tone Noise Analysis. ASME Turbo Expo. 7: Turbomachinery, Parts A, B, and C :1033-1042.
ASME paper GT2011-45886
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
TRAF
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, 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.
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.
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, 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, 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.
Transformer
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
Transition
Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2002.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Journal of Turbomachinery. 124:61–68.
Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2002.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Journal of Turbomachinery. 124:61–68.
Arnone A, Marconcini M, Pacciani R, Spano E.  2003.  Challenges in Predicting Row Interaction Effects in Axial Turbines. 33rd AIAA Fluid Dynamic Conference & Exhibit.
June 23–26, Orlando, FL, USA, AIAA paper 2003-3994

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