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An empirical model for inverted-velocity-profile jet noise prediction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stone, J. R. |
| Copyright Year | 1977 |
| 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. |
| File Size | 6706371 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780005118 |
| Archival Resource Key | ark:/13960/t4pk56118 |
| Language | English |
| Publisher Date | 1977-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Shock Waves Jet Flow Jet Aircraft Noise Aerodynamic Noise Wave Interaction Velocity Distribution Prediction Analysis Techniques Turbulent Mixing Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |