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Acoustic tests of augmentor wing model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Goodykoontz, J. H. |
| Copyright Year | 1977 |
| Description | Acoustic and aerodynamic data were obtained for a full-scale section of an augmentor wing. Features of the design included a single-row, multielement nozzle array and acoustically tuned panels placed on the interior surfaces of the augmentor. When the data were extrapolated to a 91,000-kilogram aircraft, the calculated sideline perceived noise levels were approximately the same for either the takeoff or approach condition. |
| File Size | 8440300 |
| Page Count | 57 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770015102 |
| Archival Resource Key | ark:/13960/t6353fh0b |
| Language | English |
| Publisher Date | 1977-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Augmentation Effective Perceived Noise Levels Acoustic Measurement Jet Aircraft Noise Noise Reduction Aerodynamic Noise Short Takeoff Aircraft Wing Flaps Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
