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Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shivers, J. P. Smith Jr., C. C. |
| Copyright Year | 1975 |
| Description | The investigation utilizing a small turbofan engine was conducted to evaluate static turning performance and pressure and temperature environment of an upper surface blown wing and flap segment. The tests involved modifications of the engine primary nozzle to alleviate high-temperature problems on the wing and flaps without adversely affecting static turning performance over the desired range of flap deflection and thrust condition. |
| File Size | 2036638 |
| Page Count | 41 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750008432 |
| Archival Resource Key | ark:/13960/t8qc4sr82 |
| Language | English |
| Publisher Date | 1975-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aeronautics (general) Externally Blown Flaps Exhaust Nozzles Nozzle Flow Performance Prediction Turbofan Engines Jet Flaps Aerodynamic Characteristics Lift Augmentation 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 |
