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A Computational Aeroacoustic Prediction of Discrete-Frequency Rotor-Stator Interaction Noise - a Linear Theory Analysis
Aeroacoustics
  • Scott Sawyer, The University of Akron, Main Campus
  • M. Nallasamy
  • R. Hixon
  • R. W. Dyson
Document Type
Article
Publication Date
1-1-2004
Abstract

The discrete-frequency noise generated by a rotor-stator interaction is computed by solving the fully nonlinear Euler equations in the time domain in two-dimensions. The acoustic response of the stator is determined simultaneously for the first three harmonics of the convected vertical gust of the rotor. The spatial mode generation, propagation and decay characteristics are predicted by assuming the acoustic field away from the stator can be represented as a uniform flow with small harmonic perturbations superimposed...

Citation Information
Scott Sawyer, M. Nallasamy, R. Hixon and R. W. Dyson. "A Computational Aeroacoustic Prediction of Discrete-Frequency Rotor-Stator Interaction Noise - a Linear Theory Analysis" Aeroacoustics Vol. 3 Iss. 1 (2004) p. 67 - 86
Available at: http://works.bepress.com/scott_sawyer/10/