Compressor Stage Broadband Noise Prediction using a Large-Eddy Simulation and Comparisons with a Cascade Response Model

Author:

de Laborderie Jerome1,Moreau Stephane1,Berry Alain1

Affiliation:

1. University of Sherbrooke

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. 1Ventres, C. S., Theobald, M. A., and Mark, W. D. "Turbofan noise generation - Volume 1: Analysis," Tech. Rep. CR-167952, NASA, 1982.

2. 2Goldstein, M. E., Aeroacoustics, McGraw-Hill, New York, 1976.

3. 3Hanson, D. B. "Theory for broadband noise of rotor and stator cascades with inhomogeneous inflow turbulence including effects of lean and sweep," Tech. Rep. CR-210762, NASA, East Hartford, Connecticut, USA, 2001.

4. Broadband noise prediction of fan outlet guide vane using a cascade response function

5. Laser Doppler Anemometry Measurements in an Axial Compressor Stage

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