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Design and cold-air investigation of a turbine for a small low-cost turbofan engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nusbaum, W. J. Kofskey, M. G. |
| Copyright Year | 1972 |
| Description | An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 percent of equivalent design speed and over a range of pressure ratios from 1.79 to 5.14. Presented are design information and turbine performance for first-stage and two-stage operation. Results are presented in terms of equivalent specific work, torque, mass flow, rotor exit flow angle, and efficiency. |
| File Size | 2623963 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720024422 |
| Archival Resource Key | ark:/13960/t2x39jm6r |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Auxiliary Systems Equipment Specifications Performance Tests Engine Design Compressor Efficiency Turbofan Engines Power Efficiency Cold Flow Tests Mass Flow 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 |
