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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.
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Towards structural topology optimization of rotor blisks. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 7A: Structures and Dynamics:pp.V07AT30A008;10pages.
paper GT2018-76482
Boccini E, Meli E, Rindi AA, Pinelli L, Peruzzi L, Arnone A.
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Towards structural topology optimization of rotor blisks. ASME Turbo Expo 2018: Turbine Technical Conference and Exposition. Volume 7A: Structures and Dynamics:pp.V07AT30A008;10pages.
paper GT2018-76482
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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
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