Biblio

Giovannini M, Rubechini F, Marconcini M, Arnone A, Bertini F.  2016.  Analysis of a LPT Rotor Blade For a Geared Engine. Part I: Aero-Mechanical Design and Validation. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. 2B: Turbomachinery:V02BT38A053;12pages.

Gatti G, Gaetani P, Paradiso B, Dossena V, Arcangeli L, Maceli N, Bellucci J.  2016.  An Experimental Study of the Aerodynamic Forcing Function in a 1.5 Steam Turbine Stage. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. 8: Microturbines, Turbochargers and Small Turbomachines; Steam Turbines:V008T26A020;9pages.

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.

Peruzzi L, Bellucci J, Pinelli L, Arnone A, Arcangeli L, Cosi L, Mazzucco M.  2016.  Numerical aerodynamic damping evaluation of high-pressure steam turbine blades for aeromechanical characterization. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. 8: Microturbines, Turbochargers and Small Turbomachines; Steam Turbines:V008T26A012;10pages.

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.

Pacciani R, Marconcini M, Fadai-Ghotbi A, Lardeau S, Leschziner MA.  2011.  Calculation of High-Lift Cascades in Low Pressure Turbine Conditions Using a Three-Equation Model. ASME Journal of Turbomachinery. 133(3):031016.

Pacciani R, Rubechini F, Marconcini M, Arnone A, Cecchi S, Daccà F.  2016.  A CFD-Based Throughflow Method With An Adaptive Formulation For The S2 Streamsurface. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 230(1):16-28.

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.

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.

Pacciani R, Marconcini M, Arnone A, Bertini F, Spano E, Rosa Taddei S, Sandberg R.  2024.  Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low Pressure Turbines by Means of Machine-Learnt Closures. ASME J. Turbomach.. 146(5):051009.

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.

Giovannini M, Rubechini F, Marconcini M, Arnone A, Bertini F.  2019.  Reducing Secondary Flow Losses in Low-Pressure Turbines: The “Snaked” Blade. Int. J. Turbomach. Propuls. Power. 4(3):28.

Giovannini M, Rubechini F, Marconcini M, Simoni D, Yepmo V, Bertini F.  2018.  Secondary Flows in Low-Pressure Turbines Cascades: Numerical and Experimental Investigation of the Impact of the Inner Part of the Boundary Layer. ASME Journal of Turbomachinery. 140:111002(12pages).

Ameri AA, Arnone A.  1996.  Transition Modeling Effects on Turbine Rotor Blade Heat Transfer Predictions. ASME Journal of Turbomachinery. 118(2):307–313.

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.

Pinelli L, Lori F, Marconcini M, Pacciani R, Arnone A.  2021.  Validation of a Modal Work Approach for Forced Response Analysis of Bladed Disks. Applied Sciences. 11(12):5437.