Publication Date:
2019-07-13
Description:
An empirical model for predicting the noise from inverted-velocity-profile coaxial or coannular jets is presented and compared with small-scale static and simulated flight data. The model considered the combined contributions of as many as four uncorrelated constituent sources: the premerged-jet/ambient mixing region, the merged-jet/ambient mixing region, outer-stream shock/turbulence interaction, and inner-stream shock/turbulence interaction. The noise from the merged region occurs at relatively low frequency and is modeled as the contribution of a circular jet at merged conditions and total exhaust area, with the high frequencies attenuated. The noise from the premerged region occurs at high frequency and is modeled as the contribution of an equivalent plug nozzle at outer stream conditions, with the low frequencies attenuated.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-73838
,
E-9425
,
Meeting of the Acoustical Soc. of Am.; Dec 13, 1977 - Dec 16, 1977; Miami, FL; United States
Format:
application/pdf
