On the prediction of "Buzz-saw" noise in aero-engine inlet ducts

Journal of Sound and Vibration

Volumn 248, Issue 1, 2001, Pages 123-149

  McAlpine, A ^a   Fisher, M J ^a  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE PROPAGATION; AIRCRAFT ENGINES; COMPUTER SIMULATION; FANS; INTAKE SYSTEMS; MATHEMATICAL MODELS; SUPERSONIC AERODYNAMICS; TURBULENCE; VORTEX SHEDDING;

AEROENGINE INLET DUCTS; BUZZ SAW NOISE; NONLINEAR PROPAGATION; SAWTOOTH WAVEFORM;

ACOUSTIC NOISE;

EID: 0035890874     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2001.3770     Document Type: Article

References (15)

1. The Buzz-saw noise generated by a high duty transonic compressor
2. Multiple tone generation by transonic compressors
3. A note on multiple pure tone noise
4. Shock wave behaviour in transonic compressor noise generation
5. Prediction of the spectral content of combination tone noise
6. A new look at the generation of Buzz-saw noise
7. Shock-wave radiation from a supersonic ducted rotor
8. Supersonic fan tone noise prediction
9. Theoretical models for duct acoustic propagation and radiation
10. Model equations of nonlinear acoustics
11. A recursive procedure for computing the nonlinear spectral interactions of progressive finite-amplitude waves in nondispersive fluids
12. Frequency approach to nonlinear dispersive waves