Biblio

Found 9 results
Author Keyword [ Type(Asc)] Year
Filters: Author is C Schipani  [Clear All Filters]
Conference Proceedings
Boncinelli P, Marconcini M, Poli F, Arnone A, Schipani C.  2006.  Time-Linearized Quasi-3D Tone Noise Computations in Cascade Flows. ASME Turbo Expo. 6, Turbomachinery, Parts A and B:1633–1642.
ASME paper GT2006-90080
Arnone A, Marconcini M, Pacciani R, Schipani C, Spano E.  2001.  Numerical Investigation of Airfoil Clocking in a Three-Stage Low Pressure Turbine. ASME Turbo Expo 2001: Power for Land, Sea, and Air. 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:pp.V001T03A008;9pages.
Pinelli L, Poli F, Marconcini M, Arnone A, Schipani C, Spano E, Torzo D.  2011.  A Linearized Method for Tone Noise Generation and Propagation Analysis in a Multistage Contra-Rotating Turbine. 9th European Turbomachinery Conference (ETC9). :1253–1263.
Istanbul, Turkey, 21-25 March 2011
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
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
Gambini E, Poli F, Rindi AA, Schipani C.  2005.  Robust Fluid-Solid Interfacing Algorithms with Application to Turbomachinery Aeroelastic Computations. 17th AIMeTA Congress of Theoretical and Applied Mechanics.
11-15 September 2005, Firenze, Italy
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