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Noise measurements for a twin-engine commercial jet aircraft during 3 deg approaches and level flyoversNoise measurements have been made with a twin-engine commercial jet aircraft making 3 deg approaches and level flyovers. The flight-test data showed that, in the standard 3 deg approach configuration with 40 deg flaps, effective perceived noise level (EPNL) had a value of 109.5 effective perceived noise decibels (EPNdB). This result was in agreement with unpublished data obtained with the same type of aircraft during noise certification tests; the 3 deg approaches made with 30 deg flaps and slightly reduced thrust reduced the EPNL value by 1 EPNdB. Extended center-line noise determined during the 3 deg approaches with 40 deg flaps showed that the maximum reference A-weighted sound pressure level (LA,max)ref varied from 100.0 A-weighted decibels 2.01 km (108 n. mi.) from the threshold to 87.4 db(A) at 6.12 km (3.30 n. mi.) from the threshold. These test values were about 3 db(A) higher than estimates used for comparison. The test data along the extended center line during approaches with 30 deg flaps were 1 db(A) lower than those for approaches with 40 deg flaps. Flight-test data correlating (LA,max)ref with thrust at altitudes of 122 m (400 ft) and 610 m (2000 ft) were in agreement with reference data used for comparison.
Document ID
19760019862
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hastings, E. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Shanks, R. E.
(NASA Langley Research Center Hampton, VA, United States)
Mueller, A. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1976
Subject Category
Acoustics
Report/Patent Number
NASA-TM-X-3387
L-10780
Report Number: NASA-TM-X-3387
Report Number: L-10780
Accession Number
76N26950
Funding Number(s)
PROJECT: RTOP 513-52-01-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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