Sensitivity Investigation of Aircraft Engine Noise to Operational Parameters-Reference-Cited by-同舟云学术

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Sensitivity Investigation of Aircraft Engine Noise to Operational Parameters

Published:2010-06-07 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Scarselli Gennaro¹,Paonessa Antonio²,Marulo Francesco³

Affiliation:

1. University of Salento

2. Alenia Aeronautica

3. University of Naples

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3915

Reference7 articles.

1. 2ESDU, "Computer based estimation procedure for coaxial jet noise, including far-field subsonic jet mixing noise database forstationary,coplanar conical nozzles", ItemNo.01004,ESDU Internationalplc,London,UK,May2001.

2. 3ESDU,"Prediction of noisegenerated byfansand compressorsin Turbojet and Turbofan Engines", ItemNo.98008,ESDU Internationalplc,London,UK,April1998.

3. 4Heidmann,M.F."Interimpredictionmethodforfanandcompressorsourcenoise",NASATMX-71763,1975.

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