Biblio

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, Rubechini F, Arnone A, Ibaraki S.  2006.  Numerical Investigation of a Transonic Centrifugal Compressor. ASME Turbo Expo 2006: Power for Land, Sea, and Air. 6: Turbomachinery, Parts A and B:1005-1012.

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.

Burberi C, Ghignoni E, Pinelli L, Marconcini M.  2018.  Numerical Analysis of Direct and Indirect Noise Produced by a High Pressure Turbine Stage. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:130-137.

Pinelli L, Poli F, Marconcini M, Arnone A, Schipani C, Spano E, Torzo D.  2011.  A Linearized Method for Tone Noise Generation and Propagation Analysis in a Multistage Contra-Rotating Turbine. 9th European Turbomachinery Conference (ETC9). :1253–1263.

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.

Vanti F, Agnolucci A, Pinelli L, Arnone A.  2019.  An Integrated Numerical Procedure for Flutter and Forced Response Assessment of Turbomachinery Blade-Rows. 13th European Conference on Turbomachinery Fluid dynamics & Thermodynamics ETC13.

Rubechini F, Marconcini M, Arnone A, Maritano M, Cecchi S.  2006.  The Impact of Gas Modeling in the Numerical Analysis of a Multistage Gas Turbine. ASME Turbo Expo 2006: Power for Land, Sea, and Air. 6: Turbomachinery, Parts A and B:531-539.

Boncinelli P, Maceli N, Arnone A, Rossi E.  2004.  Geometrical Effects and Coolant Injection Impact on the Performance of an HP Transonic Heavy–Duty Turbine Stage. Conf. Proc. Vol. 5: Turbo Expo 2004, Parts A and B. :1447–1457.

Giovannini M, Marconcini M, Arnone A, Bertini F.  2014.  Evaluation of Unsteady CFD Models Applied to the Analysis of a Transonic HP Turbine Stage. 10th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics (ETC 2013). :840-853.

Marconcini M, Bianchini A, Checcucci M, Biliotti D, Giachi M, Rubino D T, Arnone A, Ferrari L, Ferrara G.  2016.  Estimation of the Aerodynamic Force Induced by Vaneless Diffuser Rotating Stall in Centrifugal Compressor Stages. ATI 2016 - 71st Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 101:734-741.

Boncinelli P, Ermini M, Bartolacci S, Arnone A.  2007.  On Effects of Impeller-Diffuser Interaction in the "Radiver'' Centrifugal Compressor. ASME Turbo Expo. 6: Turbomachinery, Parts A and B:1039-1047.

Bonaiuti D, Arnone A, Hah C, Hayami H.  2002.  Development of Secondary Flow Field in a Low Solidity Diffuser in a Transonic Centrifugal Compressor Stage. ASME Turbo Expo. 5: Turbo Expo 2002, Parts A and B:445–454.

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.

Bertini F, Ampellio E, Marconcini M, Giovannini M.  2013.  A Critical Numerical Review of Loss Correlation Models and Smith Diagram for Modern Low Pressure Turbine Stages. ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. 6B: Turbomachinery:V06BT37A018-;14pages.

Facchini B, Magi A, Scotti Del Greco A.  2004.  Conjugate Heat Transfer Simulation of a Radially Cooled Gas Turbine Vane. ASME Turbo Expo 2004: Power for Land, Sea, and Air. 3:951-961.

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

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.

Arnone A, Bonaiuti D, Boncinelli P, Ermini M, Milani A, Baldassarre L, Camatti M.  2002.  CFD Applications to Industrial Centrifugal Compressor Design. ASME Turbo Expo. 5: Turbo Expo 2002, Parts A and B:639–648.

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.

Agnolucci A, Vanti F, Pinelli L, Arnone A.  2019.  Automatic Procedure for Aeromechanic Analysis of Turbomachinery Blade-Rows. 74TH ATI NATIONAL CONGRESS: Energy Conversion: Research, Innovation and Development for Industry and Territories. AIP Conference Proceedings vol. 2191:020003.

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.