Biblio

Found 437 results
Author [ Keyword(Asc)] Type Year
Filters: First Letter Of Last Name is P  [Clear All Filters]
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 
Computational Fluid Dynamics (CFD)
Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A, Spano E, Bertini F.  2026.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part II: Effect of Reynolds Number on Different Blade Geometries. ASME J Turbomach. 148(7):071002.
Computational fluid dynamics
Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2025.  The Impact of Transition and Turbulence Modelling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 10: Turbomachinery:V010T30A019.
GT2025-153288. Recommended for publication on ASME J. Turbomach.
Metti L, Marconcini M, Salvadori S, Misul DAnna, Rosafio N, Lopes G, Lavagnoli S, Fang Y, Sandberg R, Pacciani R.  2026.  The Impact of Transition and Turbulence Modeling on the SPLEEN High-Speed Low-Pressure Turbine Cascade. ASME J Turbomach. 148(2):021011.
computational aeroacoustics (CAA)
Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2023.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME J. Turbomach.. 145(8):081002.
Giaccherini S, Pinelli L, Marconcini M, Pacciani R, Arnone A.  2023.  Validation of an Analytical Model for the Acoustic Impedance Eduction of Multi-Cavity Resonant Liners by a High-Fidelity LES Approach. ASME J. Turbomach.. 145(8):081002.
Pinelli L, Marconcini M, Arnone A, Bacci D.  2024.  High Fidelity Modeling of Acoustic Liners For Aeronautical Applications. 34th Congress of the International Council of the Aeronautical Sciences.
Computation
Gatti G, Gaetani P, Paradiso B, Dossena V, Arcangeli L, Maceli N, Bellucci J.  2016.  An Experimental Study of the Aerodynamic Forcing Function in a 1.5 Steam Turbine Stage. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. 8: Microturbines, Turbochargers and Small Turbomachines; Steam Turbines:V008T26A020;9pages.
GT2016-56939
compressor
Ricci M, Pacciani R, Marconcini M, Macelloni P, Cecchi S, Bettini C.  2019.  Computational Fluid Dynamics-Based Throughflow Analysis of Transonic Flows in Steam Turbines. ASME Journal of Turbomachinery. 141(11):111005(7pages).
Pacciani R, Marconcini M, Arnone A, Bertini F, Spano E, Rosa Taddei S, Sandberg R.  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.
Rosenzweig M, Kozul M, Sandberg R, Giannini G, Pacciani R, Marconcini M, Arnone A.  2026.  Numerical Design of Experiments for Repeating Low-Pressure Turbine Stages Part I: Computational Opportunities and Methodology. ASME J Turbomach. 148(7):071001.
complex modes
Arnone A, Poli F, Schipani C.  2003.  A Method to Assess Flutter Stability of Complex Modes. 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 7–11, Durham, NC, USA
combustor-HPT interaction
Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  Understanding Entropy Wave Evolution in High-Pressure Turbines: The Role of Hot Spot Position and Features. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery:V12DT36A015.
GT2024-127446
Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  Understanding Entropy Wave Evolution in High-Pressure Turbines: The Role of Hot Spot Position and Features. ASME Turbo Expo 2024 Turbomachinery Technical Conference and Exposition. Volume 12D: Turbomachinery:V12DT36A015.
GT2024-127446
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
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
CO2-mixture
Bandini A, Arcangeli L, Paggini A, Nenciolini A, Iobbi M, Pinelli L, Marconcini M, Arnone A.  2025.  An Inquiry Into the Aerodynamic and Aeromechanic Aspects on Next-Generation CO2-SO2 Power Turbines for Sustainable Applications: The Case of the Desolination Project. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 9: Structures and Dynamics:V009T28A023.
GT2025-153814
Bandini A, Arcangeli L, Paggini A, Nenciolini A, Iobbi M, Pinelli L, Marconcini M, Arnone A.  2025.  An Inquiry Into the Aerodynamic and Aeromechanic Aspects on Next-Generation CO2-SO2 Power Turbines for Sustainable Applications: The Case of the Desolination Project. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 9: Structures and Dynamics:V009T28A023.
GT2025-153814
CNN
Pela A, Marconcini M, Arnone A, Agnolucci A, Belardini E, Valente R, Grimaldi A, Toni L.  2025.  Convolutional Neural Network Approach for Impeller Blade Loading Inference. 1st International Symposium on AI and Fluid Mechanics (AIFLUIDs).
Clocking
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
Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2002.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Journal of Turbomachinery. 124:61–68.
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
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
CFD validation
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.
CFD
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.
Barreca P, Pinelli L, Vanti F, Arnone A.  2018.  Aeroelastic Investigation of a Transonic Compressor Rotor with Multi-Row Effects. ATI 2018 - 73rd Conference of the Italian Thermal Machines Engineering Association. Energy Procedia 148:58-65.

Pages