NASA-CR-3176
A method for predicting the noise levels of coannular jets with inverted velocity profiles
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.
Subject: ACOUSTIC ATTENUATION
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:15:50Z | |
| date available | 2017-09-04T17:15:50Z | |
| date copyright | 01/01/1979 | |
| date issued | 1979 | |
| identifier other | CBIOEEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/139268 | |
| description 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. | |
| language | English | |
| title | NASA-CR-3176 | num |
| title | A method for predicting the noise levels of coannular jets with inverted velocity profiles | en |
| type | standard | |
| page | 164 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1979 | |
| contenttype | fulltext | |
| subject keywords | ACOUSTIC ATTENUATION | |
| subject keywords | EXHAUST NOZZLES | |
| subject keywords | GRAPHS (CHARTS) | |
| subject keywords | JET AIRCRAFT NOISE | |
| subject keywords | NOISE REDUCTION | |
| subject keywords | PERFORMANCE PREDICTION | |
| subject keywords | STROUHAL NUMBER | |
| subject keywords | VELOCITY DISTRIBUTION | |
| subject keywords | WIND TUNNEL TESTS |

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