Biblio

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  The Effect of Entropy Waves Features on the Indirect Noise Generation within an Aeronautical High Pressure Turbine Stage. 79th ATI National Conference.

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2024.  The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage. ASME J. Turbomach.. 146(4):041003.

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.

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.

Pinelli L, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2023.  The Effects of Swirling Flows in Entropy Wave Convection Through High Pressure Turbine Stage. ASME J. Turbomach.. 145(3):031004.

Pinelli L, Giannini G, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2023.  The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage. ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition. 13D: Turbomachinery

Pinelli L, Marconcini M, Pacciani R, Notaristefano A, Gaetani P.  2022.  The Effects of Swirling Flows In Entropy Wave Convection Through High Pressure Turbine Stage. ASME Turbo Expo 2022 Turbomachinery Technical Conference and Exposition. 10D: Turbomachinery

Peruzzi L, Bellucci J, Pinelli L, Marconcini M, Gatta G, Colatoni S, Abhimanyu S, Natale G.  2018.  Flutter-free design of aeroderivative gas turbine nozzles with simplified aero-mechanical models. 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).

Arnone A, Cattanei A, Nurzia F, Pacciani R, Zunino P.  2000.  A Two-Stage Low Pressure Gas-Turbine Model for Rotor-Stator Aerodynamic Interaction Investigations. XV Symposium of Measurement Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines.