Biblio

Biagiotti S, Pinelli L, Poli F, Vanti F, Pacciani R.  2018.  Numerical Study of Flutter Stabilization in Low Pressure Turbine Rotor with Intentional Mistuning. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association.. Energy Procedia 148:98-105.

Arnone A, Pacciani R.  1996.  Numerical Investigation on Wake Shedding in a Turbine Rotor Blade. 15th International Conference on Numerical Methods in Fluid Dynamics. :358–363.

Marconcini M, Pacciani R.  2003.  Numerical Investigation of Wake–Shock Interactions and Clocking in a Transonic HP Turbine. ASME Turbo Expo. 6: Turbo Expo 2003, Parts A and B:235–243.

Pacciani R, Spano E.  2006.  Numerical Investigation of the Effect of Roughness and Passing Wakes on LP Turbine Blades Performance. ASME Turbo Expo. Conf. Proc. Vol. 6: Turbomachinery, Parts A and B:1713–1722.

Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2001.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Turbo Expo 2001: Power for Land, Sea, and Air. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A008;9pages.

Marconcini M, Pacciani R, Arnone A, Michelassi V, Pichler R, Zhao Y, Sandberg R.  2018.  LES and RANS analysis of the end-wall flow in a linear LPT cascade with variable inlet conditions, Part II: Loss generation. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 2B: Turbomachinery:pp.V02BT41A024;11pages.

Pichler R, Zhao Y, Sandberg R, Michelassi V, Pacciani R, Marconcini M, Arnone A.  2018.  LES and RANS Analysis of the End-Wall Flow in a Linear LPT Cascade: Part I — Flow and Secondary Vorticity Fields Under Varying Inlet Condition. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 2B: Turbomachinery:pp.V02BT41A020;11pages.

Fang Y, Reissmann M, Pacciani R, Zhao Y, Ooi A, Marconcini M, Akolekar H, Sandberg R.  2024.  Exploiting a Transformer Architecture to Simultaneous Development of Transition and Turbulence Models for Turbine Flow Predictions. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12C: Turbomachinery:V12CT32A023.

Fang Y, Rosenzweig M, Reissmann M, Pacciani R, Marconcini M, Bertini F, Sandberg RD.  In Press.  Data-Driven Enhancements to Transition and Turbulence Modeling Under Varying Pressure Gradients and Unsteadiness Effects. 15th International ERCOFTAC Symposium on Engineering Turbulence Modelling and Measurements (ETMM15).

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, Fadai-Ghotbi A, Lardeau S, Leschziner MA.  2009.  Calculations of High-Lift Cascades in Low Pressure Turbine Conditions Using a Three-Equation Model. ASME Turbo Expo 2009: Power for Land, Sea, and Air. 7: Turbomachinery, Parts A and B:pp.433-442.

Pacciani R, Rubechini F, Arnone A, Lutum E.  2010.  Calculation of Steady and Periodic Unsteady Blade Surface Heat Transfer in Separated Transitional Flow. ASME Turbo Expo 2010: Power for Land, Sea, and Air. 4: Heat Transfer, Parts A and B:891-900.

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.

Pinelli L, Castelli N, Vanti F, Pacciani R, Arnone A.  2021.  Aeroelastic Investigation of an Open 3D Steam Turbine Test Case and Blade Shape Optimization with Improved Flutter Behavior. 14th European Conference on Turbomachinery Fluid dynamics.

Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2022.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. Volume 10C: Turbomachinery

Arnone A, Cattanei A, Nurzia F, Pacciani R, Zunino P.  2000.  A Two-Stage Low Pressure Gas-Turbine Model for Rotor-Stator Aerodynamic Interaction Investigations. XV Symposium of Measurement Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines.

Marconcini M, Pacciani R, Arnone A.  2015.  Transition Modelling Implications in the CFD Analysis of a Turbine Nozzle Vane Cascade Tested Over a Range of Mach and Reynolds Numbers. 12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows.

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.

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.

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.

Pacciani R, Marconcini M, Arnone A, Bertini F.  2013.  Predicting High-Lift Low-Pressure Turbine Cascades Flows Using Transition-Sensitive Turbulence Closures. ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. 6B: Turbomachinery:V06BT37A039;13pages.

Arnone A, Marconcini M, Pacciani R, Spano E.  1999.  Numerical Prediction of Wake–Induced Transition in a Low Pressure Turbine. 14th ISABE Symposium.

Arnone A, Pacciani R.  1997.  Numerical Prediction of Trailing Edge Wake Shedding. ASME Turbo Expo.

Rosenzweig M, Kozul M, Sandberg RD, 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.