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Design and fabrication of an augmentor wing model for acoustic tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Campbell, J. M. Jackson, J. Schedin, R. W. |
| Copyright Year | 1973 |
| Description | The design and fabrication of a full-scale section of an augmentor wing to be used for acoustic testing at the Lewis Research Center are discussed. This hardware will be used primarily to investigate scaling effects of acoustic data obtained during the Boeing-run model tests. Typical model test data is shown in the report, together with predictions on both performance and acoustics that can be expected from the full-scale section to be built. Areas covered include: the aerodynamic and acoustic criteria of the flap system and nozzles, detailed discussion of the hardware, test system operation procedure, and stress analysis of the entire test system. |
| File Size | 4815448 |
| Page Count | 106 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740009847 |
| Archival Resource Key | ark:/13960/t5q863099 |
| Language | English |
| Publisher Date | 1973-12-01 |
| Access Restriction | Open |
| Subject Keyword | Test Facilities Wings Noise Reduction Linings Performance Prediction Nozzles Acoustics Short Takeoff Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
