Biblio

Found 21 results
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2025
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
Innocenti G, Miris L, Pinelli L, Del Vescovo G, Beghini E, Tripoli G, Scotti Del Greco A, Marconcini M.  2025.  Aeromechanical Assessment of an Optical Probe Installed in a Two-Stage High-Pressure Gas Turbine. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T36A022.
GT2025-153843
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)
Milli L, Lottini F, Marconcini M, Arnone A.  2025.  CFD Investigation of Unsteady Interactions in a Radial-Axial Turboexpander for Geothermal Power Plant Applications. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T35A006.
GT2025-153202
Giannini G, Pinelli L, Pacciani R, Arnone A, Bertini F, Spano E, Marconcini M.  2025.  The Impact of Modeling Assumptions on the Hot Spots Convection Within a Cooled High-Pressure Turbine Stage. Aerospace Science and Technology. 166
Rosenzweig M, Kozul M, Sandberg RD, Giannini G, Pacciani R, Marconcini M, Arnone A, Spano E, Bertini F.  2025.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 2: Effect of Reynolds Number on Different Blade Geometries. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 11: Turbomachinery:V011T32A024.
GT2025-153512. Recommended for publication on ASME J. Turbomach.
Rosenzweig M, Kozul M, Sandberg RD, Giannini G, Pacciani R, Marconcini M, Arnone A, Spano E, Bertini F.  2025.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 2: Effect of Reynolds Number on Different Blade Geometries. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 11: Turbomachinery:V011T32A024.
GT2025-153512. Recommended for publication on ASME J. Turbomach.
Rosenzweig M, Kozul M, Sandberg RD, Giannini G, Pacciani R, Marconcini M, Arnone A.  2025.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part 1: Computational Opportunities and Methodology. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 11: Turbomachinery:V011T32A014.
GT2025-152583. Recommended for publication on ASME J. Turbomach.
2019
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, Peruzzi L, Arnone A, Arcangeli L, Maceli N.  2019.  Numerical and Experimental Aerodynamic Investigation of Low Pressure Steam Turbine Module. ASME Turbo Expo 2019. Volume 8: Microturbines, Turbochargers, and Small Turbomachines; Steam Turbines:V008T29A024.
ASME paper GT2019-91279
2018
Amato G, Giovannini M, Marconcini M, Arnone A.  2018.  Unsteady Methods Applied to a Transonic Aeronautical Gas Turbine Stage. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:74-81.
2015
Rubechini F, Marconcini M, Giovannini M, Bellucci J, Arnone A.  2015.  Accounting for Unsteady Interaction in Transonic Stages. ASME Journal of Engineering for Gas Turbines and Power. 137(5):1-9.
2014
Giovannini M, Marconcini M, Arnone A, Bertini F.  2014.  Evaluation of Unsteady Computational Fluid Dynamics Models Applied to the Analysis of a Transonic High-Pressure Turbine Stage. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy. 228(7):813-824.
2013
Rubechini F, Marconcini M, Arnone A, Scotti Del Greco A, Biagi R.  2013.  Special Challenges in the Computational Fluid Dynamics Modeling of Transonic Turbo-Expanders. ASME Journal of Engineering for Gas Turbines and Power. 135:102701.
ASME paper GT2013-95554
2003
Arnone A, Marconcini M, Pacciani R, Spano E.  2003.  Challenges in Predicting Row Interaction Effects in Axial Turbines. 33rd AIAA Fluid Dynamic Conference & Exhibit.
June 23–26, Orlando, FL, USA, AIAA paper 2003-3994
2001
Schmitt S, Eulitz F, Wallscheid L, Arnone A, Marconcini M.  2001.  Evaluation of Unsteady CFD Methods by Their Application to a Transonic Propfan Stage. ASME Turbo Expo 2001: Power for Land, Sea, and Air. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:V001T03A014;12pages.
2000
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.
9th ISUAAAT, September 4–8, Lyon, France