Biblio

Found 240 results
[ Author(Desc)] Keyword Type Year
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M
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.
ASME paper 2003–GT–38401
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, 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, 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, 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.
Paper No. GT2007-27200
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.
paper GT2018-76450
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.
paper n.135
Martelli F, Arnone A, Boretti A, Michelassi V.  1988.  Turbulence and Combustion Models for Turbomachinery Applications.
17 June, ERCOFTAC Meeting, Turin
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.
Dublin, Ireland, 19-20 May 1998.
P
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
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.
ASME paper GT2010-23300
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.
Pisa, Italy, 17-20 September.
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.
Paper No. GT2010-23275
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.
ASME paper GT2009-59557
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, Marconcini M, Bertini F, Rosa Taddei S, Spano E, Zhao Y, Akolekar H, Sandberg R, Arnone A.  Submitted.  Assessment of Machine-Learnt Turbulence Models Trained for Improved Wake-Mixing in Low Pressure Turbine Flows. Energies.
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.
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.
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.
Paper GT2013-95605
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.
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

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