Biblio

Found 237 results
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Tone Noise
Pinelli L, Poli F, Marconcini M, Arnone A, Spano E, Torzo D.  2011.  Validation of a 3D Linearized Method for Turbomachinery Tone Noise Analysis. ASME Turbo Expo. 7: Turbomachinery, Parts A, B, and C :1033-1042.
ASME paper GT2011-45886
Poli F, Arnone A, Schipani C.  2009.  A 3D Linearized Method for Turbomachinery Tone Noise Analysis With 3D Non-Reflecting Boundary Conditions. 8th European Turbomachinery Conference (ETC8). :713-722.
23-27 March, Graz, Austria
time-linearized
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
SPLEEN
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.  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.
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.
Metti L, Pacciani R, Rosenzweig M, Fang Y, Sandberg RD, Lavagnoli S, Marconcini M.  Submitted.  Unveiling Boundary Layer Physics in the SPLEEN High-Speed LPT with Realistic Turbulent Inflow: a Wall-Resolved LES Benchmark for RANS Models. Aerospace Science and Technology.
Roughness
Pacciani R, Spano E.  2006.  Numerical Investigation of the Effect of Roughness and Passing Wakes on LP Turbine Blades Performance. ASME Turbo Expo. Conf. Proc. Vol. 6: Turbomachinery, Parts A and B:1713–1722.
May 8–11, Barcelona, Spain, ASME paper GT2006-90221
Real Gas
Marconcini M, Rubechini F, Arnone A, Scotti Del Greco A, Biagi R.  2012.  Aerodynamic Investigation of a High Pressure Ratio Turbo-Expander for Organic Rankine Cycle Applications. ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. 8: Turbomachinery, Parts A, B, and C:847-856.
ASME paper GT2012-69409.
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
Propfan
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.

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