Arnone A, Carnevale E A, Marconcini M.
1997.
Grid Dependency Study for the NASA Rotor 37 Compressor Blade. ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A056;(9pages).
Cozzi L, Rubechini F, Marconcini M, Arnone A, Astrua P, Schneider A, Silingardi A.
2017.
Facing the Challenges in CFD Modelling of Multistage Axial Compressors. ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. 2B: Turbomachinery:pp.V02BT41A007;11pages.
ASME paper GT2017-63240
Batisti M, Marconcini M, Agnolucci A, Belardini E, Grimaldi A, Toni L, Valente R, Arnone A.
2025.
Experimental and Numerical Rotating Stall Investigation of a Multistage Centrifugal Compressor. ASME Turbo Expo 2025 Turbomachinery Technical Conference and Exposition. 12: Turbomachinery:V012T35A009.
GT2025-153766. Published on ASME J. Eng. Gas Turbine. Power
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.
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
Rubechini F, Marconcini M, Arnone A.
2008.
A CFD Model for Real Gas Effects in Turbomachinery. 8th World Congress on Computational Mechanics (WCCM8), 5th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2008).
Venezia, Italy, June 30 - July 5, 2008