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Experimental investigation of a 4 and 1/2 stage turbine with very high stage loading factor. 2: turbine performance
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Thomas, M. W. Walker, N. D. |
| Copyright Year | 1974 |
| Description | The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor are presented. A four-stage turbine was tested with and without outlet turning vanes. The 4 1/2-stage turbine achieved a design point total-to-total efficiency of 0.853. The outlet turning vane design point performance was 0.4 percent of the overall 4 1/2-stage turbine efficiency. Tests were conducted at various levels of Reynolds number and indicated decreases in turbine efficiency and equivalent weight flow with decreasing Reynolds number. |
| File Size | 40927522 |
| Page Count | 97 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740008378 |
| Archival Resource Key | ark:/13960/t1sf7jb89 |
| Language | English |
| Publisher Date | 1974-02-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Equipment Specifications Air Flow Performance Tests Propulsion System Performance Engine Design Lift Fans 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 |