Biblio

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).

Giovannini M, Marconcini M, Rubechini F, Arnone A, Bertini F.  2016.  Scaling Three-Dimensional Low-Pressure Turbine Blades for Low-Speed Testing. ASME Journal of Turbomachinery. 138(11):111001-1-9.

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.

Marconcini M, Rubechini F, Pacciani R, Arnone A, Bertini F.  2012.  Redesign of High-Lift Low Pressure Turbine Airfoils For Low Speed Testing. ASME Journal of Turbomachinery. 134(5):051017.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2014.  Predicting High-Lift Low-Pressure Turbine Cascades Flows Using Transition-Sensitive Turbulence Closures. ASME Journal of Turbomachinery. 136(5):051007.

Bertini F, Credi M, Marconcini M, Giovannini M.  2013.  A Path Toward the Aerodynamic Robust Design of Low Pressure Turbines. ASME Journal of Turbomachinery. 135:021018.

Pacciani R, Marconcini M, Arnone A, Bertini F, Spano E, Rosa Taddei S, Sandberg RD.  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.

Giovannini M, Marconcini M, Arnone A, Bertini F.  2014.  Evaluation of Unsteady Computational Fluid Dynamics Models Applied to the Analysis of a Transonic High-Pressure Turbine Stage. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 228(7):813-824.

Berrino M, Bigoni F, Simoni D, Giovannini M, Marconcini M, Pacciani R, Bertini F.  2016.  Combined Experimental and Numerical Investigations on the Roughness Effects on the Aerodynamic Performances of LPT Blades. Journal of Thermal Science. 25(1):32-42.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2011.  An Assessment of the Laminar Kinetic Energy Concept for the Prediction of High-Lift, Low-Reynolds Number Cascade Flows. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 225(7):995-1003.

Pacciani R, Marconcini M, Bertini F, Rosa Taddei S, Spano E, Zhao Y, Akolekar H, Sandberg R, Arnone A.  2021.  Assessment of Machine-Learned Turbulence Models Trained for Improved Wake-Mixing in Low Pressure Turbine Flows. Energies. 14(24):8327.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2014.  URANS Prediction of the Effects of Upstream Wakes on High-Lift LP Turbine Cascades Using Transition-Sensitive Turbulence Closures. 68th Conference of the Italian Thermal Machines Engineering Association (ATI) . Energy Procedia 45:1097-1106.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2012.  URANS Analysis of Wake-Induced Effects in High-Lift, Low Reynolds Number Cascade Flows. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:1521-1530.

Giovannini M, Rubechini F, Marconcini M, Arnone A, Bertini F.  2019.  Reducing Secondary Flow Losses in Low-Pressure Turbines: The “Snaked” Blade. 13th European Conference on Turbomachinery Fluid dynamics & Thermodynamics ETC13.

Marconcini M, Rubechini F, Pacciani R, Arnone A, Bertini F.  2010.  Redesign of High-Lift LP-Turbine Airfoils for Low Speed Testing. ASME Turbo Expo 2010: Power for Land, Sea, and Air. 7: Turbomachinery, Parts A, B, and C:909-918.

Bertini F, Credi M, Marconcini M, Giovannini M.  2012.  A Path Towards the Aerodynamic Robust Design of Low Pressure Turbines. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:pp.1497-1507.

Giovannini M, Marconcini M, Arnone A, Bertini F.  2014.  Evaluation of Unsteady CFD Models Applied to the Analysis of a Transonic HP Turbine Stage. 10th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics (ETC 2013). :840-853.

Bertini F, Ampellio E, Marconcini M, Giovannini M.  2013.  A Critical Numerical Review of Loss Correlation Models and Smith Diagram for Modern Low Pressure Turbine Stages. ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. 6B: Turbomachinery:V06BT37A018-;14pages.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2010.  A CFD Study of Low Reynolds Number Flow in High Lift Cascades. ASME Turbo Expo. 7: Turbomachinery, Parts A, B and C:1525–1534.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2011.  An Assessment of the Laminar Kinetic Energy Concept for the Prediction of High-Lift, Low-Reynolds Number Cascade Flows. 9th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics. :297-307.

Pacciani R, Marconcini M, Bertini F.  2009.  Assessment of an Intermittency Based Approach to Separated Flow Transition Predictions in Low-Reynolds Number High-Lift Cascade Flow. 8th European Turbomachinery Conference (ETC8). :141-151.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2010.  Sull'impiego del concetto di energia cinetica laminare per la previsione della transizione per separazione in profili high-lift per turbine aeronautiche di bassa pressione. 65o Congresso Nazionale ATI.

Giovannini M, Rubechini F, Marconcini M, Simoni D, Yepmo V, Bertini F.  2018.  Secondary Flows in LPT Cascades: Numerical and Experimental Investigation of the Impact of the Inner Part of the Boundary Layer. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 2B: Turbomachinery:pp.V02BT41A027;13pages.

Giovannini M, Marconcini M, Rubechini F, Arnone A, Bertini F.  2015.  Scaling 3D Low-Pressure Turbine Blades for Low-Speed Testing. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. 2B: Turbomachinery

Giovannini M, Rubechini F, Amato G, Arnone A, Simoni D, Yepmo V, Satta F, Bertini F.  2019.  Reducing Secondary Flow Losses in Low-Pressure Turbines With Blade Fences. Part II: Experimental Validation on Linear Cascades. ASME Turbo Expo 2019. Volume 2B: Turbomachinery:V02BT40A021.