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Static noise tests on augmentor wing jet stol research aircraft (c8a buffalo)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Marrs, C. C. Okeefe, J. V. Harkonen, D. L. |
| Copyright Year | 1974 |
| Description | Results are presented for full scale ground static acoustic tests of over-area conical nozzles and a lobe nozzle installed on the Augmentor Wing Jet STOL Research Aircraft, a modified C8A Buffalo. The noise levels and spectrums of the test nozzles are compared against those of the standard conical nozzle now in use on the aircraft. Acoustic evaluations at 152 m (500 ft), 304 m (1000 ft), and 1216 m (4000 ft) are made at various engine power settings with the emphasis on approach and takeoff power. Appendix A contains the test log and propulsion calculations. Appendix B gives the original test plan, which was closely adhered to during the test. Appendix C describes the acoustic data recording and reduction systems, with calibration details. |
| File Size | 5556485 |
| Page Count | 98 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740025342 |
| Archival Resource Key | ark:/13960/t20c9qr41 |
| Language | English |
| Publisher Date | 1974-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Acoustic Measurement Acoustic Properties Nozzle Flow Data Acquisition Lift Devices Aerodynamic Noise Data Processing Short Takeoff Aircraft Lift Augmentation Sound Pressure Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
