Nonlinear Propagation of Supersonic Fan Tones in Turbofan Intake Ducts-Reference-Cited by-同舟云学术

Nonlinear Propagation of Supersonic Fan Tones in Turbofan Intake Ducts

Published:2018-01 Issue:1 Volume:56 Page:316-328
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Adetifa Oluwaseun E.¹,McAlpine Alan¹,Gabard Gwénaël¹

Affiliation:

1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom

Funder

Engineering and Physical Science Research Council and Rolls–Royce plc

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056121

Reference21 articles.

1. Aircraft noise reduction technologies: A bibliographic review

2. HubbardH. H., Aeroacoustics of Flight Vehicles: Theory and Practice, Vol. 1, Noise Sources, American Inst. of Physics, Woodbury, MN, 1995, pp. 1–443.

3. ON THE PREDICTION OF “BUZZ-SAW” NOISE IN AERO-ENGINE INLET DUCTS

4. Modelling the Nonlinear Sound Propagation and Radiation of Supersonic Fan Tones

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