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Performance of low-pressure-ratio fan stage at two off-design blade setting angles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kovich, G. Moore, R. D. Tysl, E. R. |
| Copyright Year | 1977 |
| Description | The overall and blade-element performance of a low pressure ratio, low tip speed fan stage at design speed is presented for tow off-design rotor blade angle settings. The rotor design tip speed is 243.8 m/sec and weight flow per unit annulus area is 175.8 kg/sec. Design weight flow and pressure ratio are 29.9 kg/sec and 1.151, respectively. |
| File Size | 14833820 |
| Page Count | 91 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770013087 |
| Archival Resource Key | ark:/13960/t13n6z34p |
| Language | English |
| Publisher Date | 1977-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Fans Compressor Rotors Engine Design Rotor Blades Turbomachinery Aircraft Engines Short Haul Aircraft Tip Speed Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |