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, Bonaiuti D, Focacci A, Pacciani R, Scotti Del Greco A, Spano E.  2004.  Parametric Optimization of a High-Lift Turbine Vane. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1469–1479.

Giaccherini S, Mariotti F, Pinelli L, Marconcini M, Bianchini A.  2020.  On the Prospects of Improving the Numerical Analysis of Symmetric Airfoils at Low Reynolds Numbers and High Angles of Attack by a LES Approach: The Case of NACA0021 Profile. 75th National ATI Congress – #7 Clean Energy for all (ATI 2020). E3S Web Conf. Volume 197:08015(12).

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.

Pinelli L, Poli F, Arnone A, D’Ettole A G, Rosso E, Sartor G, Kharyton V.  2024.  The Role of Operating Conditions on Flutter Instability of a Low-Pressure Turbine Rotor. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 10A: Structures and Dynamics:V10AT21A014.

Pinelli L, Poli F, Arnone A, D’Ettole A G, Rosso E, Sartor G, Kharyton V.  2024.  The Role of Operating Conditions on Flutter Instability of a Low-Pressure Turbine Rotor. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 10A: Structures and Dynamics:V10AT21A014.

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.

Pacciani R, Rossi E.  2002.  Simulazione degli Effetti di Alcuni Parametri Progettuali sull'Interazione Statore-Rotore in uno Stadio di Turbina HP. 57o Congresso Nazionale ATI. :IV–B27–33.

Pinelli L, Malcaus M, Giannini G, Marconcini M.  2025.  Some Experiences About the RANS Modeling of UHBR Fan: The Case of ECL5/CATANA. 16th European Turbomachinery Conference ETC16.

Arnone A, Pacciani R.  1995.  Three-Dimensional Viscous Analysis of Centrifugal Impellers Using the Incompressible Navier-Stokes Equations. 1st European Conference on Turbomachinery. :181–195.

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.

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  Understanding Entropy Wave Evolution in High-Pressure Turbines: The Role of Hot Spot Position and Features. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery:V12DT36A015.

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  Understanding Entropy Wave Evolution in High-Pressure Turbines: The Role of Hot Spot Position and Features. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery:V12DT36A015.

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.

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.

Marconcini M, Pacciani R, Arnone A.  2010.  URANS Predictions of the Effects of Synthetic Jets on the Separated, Transitional Flow Over a Low-Pressure-Turbine-Like Flat Plate. ASME Turbo Expo. 7: Turbomachinery, Parts A, B and C:2605–2613.

Arnone A, Marconcini M, Pacciani R.  2000.  On the Use of Unsteady Methods in Predicting Stage Aerodynamic Performance. 9th ISUAAAT, Unsteady Aerodynamics, Aeroacustics and Aeroelasticity of Turbomachines. :24–36.

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.

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.

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.

Innocenti G, Marconcini M, Michelassi V, Ciani A, Jurek T, Scotti Del Greco A, Pacciani R.  2025.  On the Assessment of CFD Assumptions for the Preliminary Design of a Two-Stage High-Pressure Turbine: Impact of Unsteady Effects on Thermal Loads. Int. J. Heat Mass Transf. 236(1)

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.  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.

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.

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.