Biblio

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.

Marconcini M, Rubechini F, Arnone A, Scotti Del Greco A, Biagi R.  2012.  Aerodynamic Investigation of a High Pressure Ratio Turbo-Expander for Organic Rankine Cycle Applications. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:847-856.

Marconcini M, Rubechini F, Arnone A, Ibaraki S.  2008.  Design and Off-Design Numerical Investigation of a Transonic Double-Splitter Centrifugal Compressor. ASME Turbo Expo. Conf. Proc. Vol. 6: Turbomachinery, Parts A and B, and C:1571–1578.

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.

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.

Marconcini M, Bianchini A, Checcucci M, Ferrara G, Arnone A, Ferrari L, Biliotti D, Rubino D T.  2017.  A Three-Dimensional Time-Accurate Computational Fluid Dynamics Simulation of the Flow Field Inside a Vaneless Diffuser During Rotating Stall Conditions. ASME Journal of Turbomachinery. 139(2):021001.

Marconcini M, Rubechini F, Arnone A, Ibaraki S.  2007.  Numerical Analysis of the Vaned Diffuser of a Transonic Centrifugal Compressor. ASME Turbo Expo 2007: Power for Land, Sea, and Air. 6: Turbo Expo 2007, Parts A and B:987-995.

Marconcini M, Rubechini F, Arnone A, Ibaraki S.  2010.  Numerical Analysis of the Vaned Diffuser of a Transonic Centrifugal Compressor. ASME Journal of Turbomachinery. 132:041012.

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.

Marconcini M, Pacciani R, Arnone A, Michelassi V, Pichler R, Zhao Y, Sandberg R.  2019.  Large Eddy Simulation and RANS Analysis of the End-Wall Flow in a Linear Low-Pressure-Turbine Cascade - Part II: Loss Generation. ASME Journal of Turbomachinery. 141(5):051004(9pages).

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.

Mariotti F, Lilli L, Pinelli L, Arcangeli L, Maceli N, Brazzini F, Marconcini M, Arnone A.  2023.  Simulating Part-Span Snubber in Low Pressure Steam Turbine Rotor With Simplified Methods for Aerodynamic and Aeromechanical Assessment. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 10: Steam Turbine

Martelli F, Arnone A, Boretti A, Michelassi V.  1988.  Turbulence and Combustion Models for Turbomachinery Applications.

Mosele S G, Garbarino T, Schneider A, Cozzi L, Arnone A, Goinis G, Hedkvist S.  2019.  Compressor Retrofittable Solutions in Heavy-Duty Gas Turbines for Minimum Environmental Load Reduction. SUPEHR19 SUstainable PolyEnergy generation and HaRvesting. 113

Munari A, Motta A, Spano E, Boncinelli P, Arnone A.  1998.  Oxygen Inducer Design and Test Analysis. CNES/ESA International Conference on Spacecraft Propulsion.

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.

Pacciani R, Fang Y, Metti L, Marconcini M, Sandberg RD.  2024.  A Reformulation of the Laminar Kinetic Energy Model to Enable Multi-Mode Transition Predictions.. Flow, Turbulence and Combustion. s10494-024-00590-y

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, 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.

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.

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.

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.  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, 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, Marconcini M, Arnone A, Bertini F, Spano E, Rosa Taddei S, Sandberg RD.  2023.  Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low Pressure Turbines by Means of Machine-Learnt Closures. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13B: Turbomachinery