Aeroelastic Investigation of a Transonic Compressor Rotor with Multi-Row Effects

Author:

Barreca Pietro,Pinelli Lorenzo,Vanti Federico,Arnone Andrea

Publisher

Elsevier BV

Reference6 articles.

1. Pinelli L., Poli F., Arnone A. & Schipani C., “A time-accurate 3D method for turbomachinery blade flutter analysis”, In 12th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT), (2009). September 1-4, London, UK.

2. Poli F., Pinelli L., Arnone A., “Aeroelastic stability analysis of a non-rotating annular turbine test rig: a comparison between a linearized and a non-linear computational method”, 22nd International Congress on Sound and Vibration, (ICSV22), (2015). July 12-16, Florence, Italy.

3. May M., Mauffrey Y., & Sicot F., “Numerical flutter analysis of turbomachinery blading based on time-linearized, time-spectral and time-accurate simulations”, In 15th International Forum on Aeroelasticity and Structural Dynamics (IFASD), (2011) June 26-30. Paris, France.

4. Chenaux V.A., Grüber B., “Aeroelastic Investigations of an Annular Transonic Compressor Cascade: Numerical Sensitivity Study for Validation Purposes”, Proceedings of ASME Turbo Expo Conference 2015, (2015), Montreal, Canada.

5. Chenaux V.A., Zanker A., Ott P., “Aeroelastic Investigations of an Annular Transonic Compressor Cascade: Experimental Results”, Proceedings of ASME Turbo Expo Conference 2015, (2015), Montreal, Canada.

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