Effects of inflow distortion profiles on fan tone noise calculated using a 3-D theory
Abstract
Calculations of the fan tone acoustic power and modal structure generated by complex distortions in axial inflow velocity are presented. The model used treats the motor as a rotating three-dimensional cascade and calculates the acoustic field from the distortion-produced dipole distribution on the blades including noncompact source effects. Radial and circumferential distortion shapes are synthesized from Fourier-Bessel components representing individual distortion modes. The relation between individual distortion modes and the generated acoustic modes is examined for particular distortion cases. Comparisons between theoretical and experimental results for distortions produced by wakes from upstream radial rods show that the analysis is a good predictor of acoustic power dependence on disturbance strength.
- Publication:
-
Presented at the 5th Aeroacoustics Conf
- Pub Date:
- 1979
- Bibcode:
- 1979aeac.conf...12K
- Keywords:
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- Flow Distortion;
- Inlet Flow;
- Noise Measurement;
- Turbofans;
- Analysis (Mathematics);
- Axial Flow;
- Fourier-Bessel Transformations;
- Mathematical Models;
- Modal Response;
- Pitch;
- Rotors;
- Acoustics