Biblio

Found 11 results
Author Keyword [ Type(Asc)] Year
Filters: First Letter Of Keyword is F and Author is Andrea Arnone  [Clear All Filters]
Journal Article
Pinelli L, Lori F, Marconcini M, Pacciani R, Arnone A.  2021.  Validation of a Modal Work Approach for Forced Response Analysis of Bladed Disks. Applied Sciences. 11(12):5437.
Pinelli L, Lori F, Marconcini M, Pacciani R, Arnone A.  2021.  Validation of a Modal Work Approach for Forced Response Analysis of Bladed Disks. Applied Sciences. 11(12):5437.
Rubechini F, Marconcini M, Arnone A, Maritano M, Cecchi S.  2008.  The Impact of Gas Modeling in the Numerical Analysis of a Multistage Gas Turbine. ASME Journal of Turbomachinery. 130(2):021022.
Sláma V, Rudas B, Eret P, Tsymbalyuk V, Ira J, Macalka A, Pinelli L, Vanti F, Arnone A, Lo Balbo A A.  2018.  Experimental and Numerical Study of Controlled Flutter Testing in a Linear Turbine Blade Cascade. Acta Polytechnica CTU Proceedings. Vol 20 Turbomachines 2018:98-107.
Conference Proceedings
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.
paper ETC2019-199
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.
paper ETC2019-199
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.
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.
Conference Paper
Pinelli L, Poli F, Arnone A, Schipani C.  2009.  A Time-Accurate 3D Method for Turbomachinery Blade Flutter Analysis. 12th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 1–4, London, UK. paper I12-S8-3
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
Poli F, Gambini E, Arnone A, Schipani C.  2006.  A 3D Time-Linearized Method for Turbomachinery Blade Flutter Analysis. 11th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT).
September 4–8, Moscow, Russia