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Advanced subsonic transport approach noise: The relative contribution of airframe noiseWith current engine technology, airframe noise is a contributing source for large commercial aircraft on approach, but not the major contributor. With the promise of much quieter jet engines with the planned new generation of high-by-pass turbofan engines, airframe noise has become a topic of interest in the advanced subsonic transport research program. The objective of this paper is to assess the contribution of airframe noise relative to the other aircraft noise sources on approach. The assessment will be made for a current technology large commercial transport aircraft and for an envisioned advanced technology aircraft. NASA's Aircraft Noise Prediction Program (ANOPP) will be used to make total aircraft noise predictions for these two aircraft types. Predicted noise levels and areas of noise contours will be used to determine the relative importance of the contributing approach noise sources. The actual set-up decks used to make the ANOPP runs for the two aircraft types are included in appendixes.
Document ID
19920024904
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Willshire, William L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Garber, Donald P.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:104112
NASA-TM-104112
Report Number: NAS 1.15:104112
Report Number: NASA-TM-104112
Accession Number
92N34148
Funding Number(s)
PROJECT: RTOP 537-03-21-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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