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Single-stage experimental evaluation of compressor blading with slots and vortex generators, part 5
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Brent, J. A. |
| Copyright Year | 1972 |
| Description | An experimental investigation was conducted to determine the extent that slots and vortex generators can increase the efficiency and stable operating range of highly loaded compressor stages. With slots in the rotor and stator, the stage performance both with and without vortex generators was inferior to that achieved with the unslotted blading. However, with vortex generators, stator slots, and an unslotted rotor, the stable operating range increased 25% and the stage peak efficiency increased 2.1% over the values achieved with the unslotted rotor and stator without vortex generators, at design equivalent rotor speed. |
| File Size | 10193422 |
| Page Count | 133 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720015141 |
| Archival Resource Key | ark:/13960/t0cv98h5p |
| Language | English |
| Publisher Date | 1972-03-31 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Equipment Specifications Propulsion System Performance Engine Design Turbine Wheels Vortex Generators Engine Tests Turbine Engines 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 |
