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Effects of motion on jet exhaust noise from aircraftThe various problems involved in the evaluation of the jet noise field prevailing between an observer on the ground and an aircraft in flight in a typical takeoff or landing approach pattern were studied. Areas examined include: (1) literature survey and preliminary investigation, (2) propagation effects, (3) source alteration effects, and (4) investigation of verification techniques. Sixteen problem areas were identified and studied. Six follow-up programs were recommended for further work. The results and the proposed follow-on programs provide a practical general technique for predicting flyover jet noise for conventional jet nozzles.
Document ID
19760021872
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chun, K. S.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Berman, C. H.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Cowan, S. J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Publication Information
Publisher: NASA
Subject Category
Acoustics
Report/Patent Number
NASA-CR-2701
D6-41995
Report Number: NASA-CR-2701
Report Number: D6-41995
Accession Number
76N28960
Funding Number(s)
CONTRACT_GRANT: NAS3-18539
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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