Biblio

Found 24 results
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Conference Paper
Agnolucci A, Marconcini M, Arnone A, Toni L, Grimaldi A, Giachi M.  2021.  Centrifugal Compressor Stage Efficiency and Rotor Stiffness Augmentation via Artificial Neural Networks. ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition. 2D: Turbomachinery: Radial Turbomachinery Aerodynamics
ASME paper GT2021-59998
Bellucci J, Rubechini F, Marconcini M, Arnone A, Arcangeli L, Maceli N, Dossena V.  2014.  The Influence of Roughness on a High-Pressure Steam Turbine Stage: an Experimental and Numerical Study. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. 1B: Marine; Microturbines, Turbochargers and Small Turbomachines; Steam Turbines:V01BT27A015;12pages.
ASME paper GT2014-25540
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.
Domus de Maria (CA), Italy, 13-17 Settembre 2010, articolo 12-084
Conference Proceedings
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.
23-27 March, Graz, Austria
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.
ASME paper GT2008-50759
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.
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.
ASME paper GT2007-27235
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.
ASME paper GT2007-27235
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.
ASME paper GT2010-23297
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.
ASME paper GT2010-23297
Journal Article
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.
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.
winner of 2011 SAGE Best Paper Award (JPE) http://pia.sagepub.com/cgi/collection/2011
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, Marconcini M, Arnone A.  2019.  Comparison of the AUSM+-up and Other Advection Schemes for Turbomachinery Applications. Shock Waves. 29(5):705-716.
Bellucci J, Rubechini F, Marconcini M, Arnone A, Arcangeli L, Maceli N, Dossena V.  2015.  The Influence of Roughness on a High-Pressure Steam Turbine Stage: an Experimental and Numerical Study. ASME Journal of Engineering for Gas Turbines and Power. 137(1):1-9.
Bellucci J, Rubechini F, Marconcini M, Arnone A, Arcangeli L, Maceli N, Dossena V.  2015.  The Influence of Roughness on a High-Pressure Steam Turbine Stage: an Experimental and Numerical Study. ASME Journal of Engineering for Gas Turbines and Power. 137(1):1-9.
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).
Pichler R, Zhao Y, Sandberg R, Michelassi V, Pacciani R, Marconcini M, Arnone A.  2019.  Large-Eddy Simulation and RANS Analysis of the End-Wall Flow in a Linear Low-Pressure Turbine Cascade, Part I: Flow and Secondary Vorticity Fields Under Varying Inlet Condition. ASME Journal of Turbomachinery. 141(12):121005(10pages).
Marconcini M, Rubechini F, Arnone A, Ibaraki S.  2008.  Numerical Investigation of a Transonic Centrifugal Compressor. ASME Journal of Turbomachinery. 130(1):011010.
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.
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.
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.
Riccietti E, Bellucci J, Checcucci M, Marconcini M, Arnone A.  2018.  Support Vector Machine Classification Applied to the Parametric Design of Centrifugal Pumps. Engineering Optimization. 50(8):1304-1324.
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. Journal of Thermal Science. 24(6):526-534.