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Redesigned rotor for a highly loaded, 1800 ft/sec tip speed compressor fan stage 1: aerodynamic and mechanical design
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Halle, J. E. Ruschak, J. T. |
| Copyright Year | 1975 |
| Description | A highly loaded, high tip-speed fan rotor was designed with multiple-circular-arc airfoil sections as a replacement for a marginally successful rotor which had precompression airfoil sections. The substitution of airfoil sections was the only aerodynamic change. Structural design of the redesigned rotor blade was guided by successful experience with the original blade. Calculated stress levels and stability parameters for the redesigned rotor are within limits demonstrated in tests of the original rotor. |
| File Size | 17145762 |
| Page Count | 62 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760003045 |
| Archival Resource Key | ark:/13960/t0vq7qd9v |
| Language | English |
| Publisher Date | 1975-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Structural Design Airfoils Compressor Rotors Rotor Blades Turbomachinery Aerodynamic Loads Tip Speed 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 |
