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Assessment of NASA's Aircraft Noise Prediction CapabilityA goal of NASA s Fundamental Aeronautics Program is the improvement of aircraft noise prediction. This document provides an assessment, conducted from 2006 to 2009, on the current state of the art for aircraft noise prediction by carefully analyzing the results from prediction tools and from the experimental databases to determine errors and uncertainties and compare results to validate the predictions. The error analysis is included for both the predictions and the experimental data and helps identify where improvements are required. This study is restricted to prediction methods and databases developed or sponsored by NASA, although in many cases they represent the current state of the art for industry. The present document begins with an introduction giving a general background for and a discussion on the process of this assessment followed by eight chapters covering topics at both the system and the component levels. The topic areas, each with multiple contributors, are aircraft system noise, engine system noise, airframe noise, fan noise, liner physics, duct acoustics, jet noise, and propulsion airframe aeroacoustics.
Document ID
20120012957
Acquisition Source
Glenn Research Center
Document Type
Technical Publication (TP)
Authors
Dahl, Milo D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 26, 2013
Publication Date
July 1, 2012
Subject Category
Acoustics
Report/Patent Number
NASA/TP-2012-215653
E-15800
Report Number: NASA/TP-2012-215653
Report Number: E-15800
Funding Number(s)
WBS: WBS 561581.02.08.03.18.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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