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NASA-CR-3176

A method for predicting the noise levels of coannular jets with inverted velocity profiles

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1979

Abstract: A coannular jet was equated with a single stream equivalent jet with the same mass flow, energy, and thrust. The acoustic characteristics of the coannular jet were then related to the acoustic characteristics of the single jet. Forward flight effects were included by incorporating a forward exponent, a Doppler amplification factor, and a Strouhal frequency shift. Model test data, including 48 static cases and 22 wind tunnel cases, were used to evaluate the prediction method. For the static cases and the low forward velocity wind tunnel cases, the spectral mean square pressure correlation coefficients were generally greater than 90 percent, and the spectral sound pressure level standard deviation were generally less than 3 decibels. The correlation coefficient and the standard deviation were not affected by changes in equivalent jet velocity. Limitations of the prediction method are also presented.
URI: http://yse.yabesh.ir/std/handle/yse/139268
Subject: ACOUSTIC ATTENUATION
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    NASA-CR-3176

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:15:50Z
date available2017-09-04T17:15:50Z
date copyright01/01/1979
date issued1979
identifier otherCBIOEEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/139268
description abstractA coannular jet was equated with a single stream equivalent jet with the same mass flow, energy, and thrust. The acoustic characteristics of the coannular jet were then related to the acoustic characteristics of the single jet. Forward flight effects were included by incorporating a forward exponent, a Doppler amplification factor, and a Strouhal frequency shift. Model test data, including 48 static cases and 22 wind tunnel cases, were used to evaluate the prediction method. For the static cases and the low forward velocity wind tunnel cases, the spectral mean square pressure correlation coefficients were generally greater than 90 percent, and the spectral sound pressure level standard deviation were generally less than 3 decibels. The correlation coefficient and the standard deviation were not affected by changes in equivalent jet velocity. Limitations of the prediction method are also presented.
languageEnglish
titleNASA-CR-3176num
titleA method for predicting the noise levels of coannular jets with inverted velocity profilesen
typestandard
page164
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1979
contenttypefulltext
subject keywordsACOUSTIC ATTENUATION
subject keywordsEXHAUST NOZZLES
subject keywordsGRAPHS (CHARTS)
subject keywordsJET AIRCRAFT NOISE
subject keywordsNOISE REDUCTION
subject keywordsPERFORMANCE PREDICTION
subject keywordsSTROUHAL NUMBER
subject keywordsVELOCITY DISTRIBUTION
subject keywordsWIND TUNNEL TESTS
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DSpace software copyright © 2017-2020  DuraSpace
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